From c5d5987bb836c270f344a8810bac548a7cdef239 Mon Sep 17 00:00:00 2001 From: WallyMaier Date: Tue, 27 Apr 2021 10:52:47 -0700 Subject: [PATCH 1/2] Fixing version numbers to a consistent place --- Common/src/linear_algebra/blas_structure.cpp | 2 +- SU2_CFD/include/integration/CIntegrationFactory.hpp | 2 +- SU2_CFD/include/numerics/NEMO/convection/ausm.hpp | 1 - SU2_CFD/include/numerics/NEMO/convection/ausmpwplus.hpp | 1 - SU2_CFD/include/numerics/NEMO/convection/lax.hpp | 1 - SU2_CFD/include/solvers/CSolverFactory.hpp | 2 +- SU2_CFD/include/variables/CNEMOEulerVariable.hpp | 1 - SU2_CFD/include/variables/CNEMONSVariable.hpp | 1 - SU2_CFD/src/output/CNEMOCompOutput.cpp | 2 +- SU2_CFD/src/solvers/CEulerSolver.cpp | 1 - SU2_PY/convert_to_csv.py | 2 +- SU2_PY/pySU2/pySU2ad.i | 2 +- SU2_PY/updateHistoryMap.py | 2 +- TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg | 2 +- .../coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg | 2 +- TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg | 2 +- .../coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg | 2 +- .../deformation/intersection_prevention/def_intersect.cfg | 2 +- TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg | 2 +- TestCases/disc_adj_rans/cylinder/cylinder.cfg | 4 ++-- TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg | 4 ++-- TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg | 4 ++-- TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg | 4 ++-- TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg | 4 ++-- TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg | 2 +- .../transonic_stator_2D/transonic_stator.cfg | 4 ++-- TestCases/euler/bluntbody/blunt.cfg | 2 +- TestCases/fea_fsi/Airfoil_RBF/config.cfg | 2 +- TestCases/fea_fsi/SquareCyl_Beam/config.cfg | 2 +- TestCases/fixed_cl/naca0012/inv_NACA0012.cfg | 2 +- TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg | 2 +- .../streamwise_periodic/chtPinArray_2d/configFluid.cfg | 2 +- .../incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg | 2 +- TestCases/mms/dg_ringleb/ringleb_dg.cfg | 2 +- TestCases/navierstokes/poiseuille/profile_poiseuille.cfg | 4 ++-- TestCases/nicf/LS89/turb_SA_PR.cfg | 2 +- TestCases/nicf/LS89/turb_SST_PR.cfg | 2 +- .../thermalbath/finitechemistry/thermalbath.cfg | 4 ++-- .../nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg | 2 +- .../optimization_euler/steady_inverse_design/inv_NACA0012.cfg | 2 +- TestCases/rans/naca0012/turb_NACA0012_sa.cfg | 4 ++-- TestCases/rans/naca0012/turb_NACA0012_sa_binary.cfg | 4 ++-- TestCases/rans/naca0012/turb_NACA0012_sa_neg.cfg | 4 ++-- TestCases/rans/naca0012/turb_NACA0012_sst.cfg | 2 +- TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg | 2 +- TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg | 2 +- TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg | 2 +- TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg | 2 +- TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg | 2 +- TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg | 2 +- TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg | 2 +- TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg | 4 ++-- TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg | 4 ++-- TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg | 4 ++-- TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg | 4 ++-- TestCases/sliding_interface/channel_3D/zone_1.cfg | 4 ++-- TestCases/sliding_interface/channel_3D/zone_2.cfg | 4 ++-- TestCases/sliding_interface/channel_3D/zone_3.cfg | 4 ++-- TestCases/sliding_interface/incompressible_steady/config.cfg | 2 +- .../sliding_interface/incompressible_steady/configCircle.cfg | 2 +- .../sliding_interface/incompressible_steady/configOut.cfg | 2 +- .../sliding_interface/incompressible_unsteady/config.cfg | 2 +- .../incompressible_unsteady/configCircle.cfg | 2 +- .../sliding_interface/incompressible_unsteady/configOut.cfg | 2 +- TestCases/sliding_interface/pipe/pipe_NN.cfg | 4 ++-- TestCases/sliding_interface/pipe/pipe_WA.cfg | 4 ++-- TestCases/sliding_interface/pipe/zone_1.cfg | 4 ++-- TestCases/sliding_interface/pipe/zone_2.cfg | 4 ++-- TestCases/sliding_interface/pipe/zone_3.cfg | 4 ++-- TestCases/sliding_interface/pipe/zone_4.cfg | 4 ++-- TestCases/sliding_interface/pipe/zone_5.cfg | 4 ++-- .../sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg | 4 ++-- .../sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg | 4 ++-- TestCases/sliding_interface/single_stage/single_stage_NN.cfg | 4 ++-- TestCases/sliding_interface/single_stage/single_stage_WA.cfg | 4 ++-- TestCases/sliding_interface/single_stage/zone_1.cfg | 4 ++-- TestCases/sliding_interface/single_stage/zone_2.cfg | 4 ++-- .../supersonic_vortex_shedding/sup_vor_shed_NN.cfg | 4 ++-- .../supersonic_vortex_shedding/sup_vor_shed_WA.cfg | 4 ++-- .../sliding_interface/supersonic_vortex_shedding/zone_1.cfg | 4 ++-- .../sliding_interface/supersonic_vortex_shedding/zone_2.cfg | 4 ++-- TestCases/sliding_interface/uniform_flow/uniform_NN.cfg | 4 ++-- TestCases/sliding_interface/uniform_flow/uniform_WA.cfg | 4 ++-- TestCases/sliding_interface/uniform_flow/zone_1.cfg | 4 ++-- TestCases/sliding_interface/uniform_flow/zone_2.cfg | 4 ++-- TestCases/turbomachinery/APU_turbocharger/Jones.cfg | 2 +- TestCases/turbomachinery/APU_turbocharger/Jones_rst.cfg | 2 +- TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg | 2 +- TestCases/turbomachinery/axial_stage_2D/zone_1.cfg | 2 +- TestCases/turbomachinery/axial_stage_2D/zone_2.cfg | 2 +- .../turbomachinery/centrifugal_blade/centrifugal_blade.cfg | 4 ++-- .../turbomachinery/centrifugal_stage/centrifugal_stage.cfg | 2 +- .../turbomachinery/transonic_stator_2D/transonic_stator.cfg | 4 ++-- .../transonic_stator_2D/transonic_stator_rst.cfg | 4 ++-- configure.ac | 2 +- externals/tecio/Makefile.am | 2 +- 96 files changed, 132 insertions(+), 138 deletions(-) diff --git a/Common/src/linear_algebra/blas_structure.cpp b/Common/src/linear_algebra/blas_structure.cpp index a1616ff0ee5..6854354ec84 100644 --- a/Common/src/linear_algebra/blas_structure.cpp +++ b/Common/src/linear_algebra/blas_structure.cpp @@ -3,7 +3,7 @@ * \brief Implementation of the functions that either simulate BLAS functionality or interface to an actual BLAS implementation. * \author E. van der Weide - * \version 6.0.1 "Cardinal" + * \version 7.1.1 "Blackbird" * * SU2 Project Website: https://su2code.github.io * diff --git a/SU2_CFD/include/integration/CIntegrationFactory.hpp b/SU2_CFD/include/integration/CIntegrationFactory.hpp index e90f68f7abf..bb406ae2092 100644 --- a/SU2_CFD/include/integration/CIntegrationFactory.hpp +++ b/SU2_CFD/include/integration/CIntegrationFactory.hpp @@ -2,7 +2,7 @@ * \file CIntegrationFactory.hpp * \brief Headers of the CIntegrationFactory class * \author T. Albring - * \version 7.0.1 "Blackbird" + * \version 7.1.1 "Blackbird" * * SU2 Project Website: https://su2code.github.io * diff --git a/SU2_CFD/include/numerics/NEMO/convection/ausm.hpp b/SU2_CFD/include/numerics/NEMO/convection/ausm.hpp index 8e44d286e91..2a087dc7674 100644 --- a/SU2_CFD/include/numerics/NEMO/convection/ausm.hpp +++ b/SU2_CFD/include/numerics/NEMO/convection/ausm.hpp @@ -34,7 +34,6 @@ * \brief Class for solving an approximate Riemann AUSM. * \ingroup ConvDiscr * \author F. Palacios, S.R. Copeland, W. Maier, C. Garbacz - * \version 7.0.8 'Blackbird' */ class CUpwAUSM_NEMO : public CNEMONumerics { private: diff --git a/SU2_CFD/include/numerics/NEMO/convection/ausmpwplus.hpp b/SU2_CFD/include/numerics/NEMO/convection/ausmpwplus.hpp index 817f935660d..1bc53834941 100644 --- a/SU2_CFD/include/numerics/NEMO/convection/ausmpwplus.hpp +++ b/SU2_CFD/include/numerics/NEMO/convection/ausmpwplus.hpp @@ -34,7 +34,6 @@ * \brief Class for solving an approximate Riemann AUSM. * \ingroup ConvDiscr * \author F. Palacios, W.Maier, C. Garbacz - * \version 7.0.8 "Falcon" */ class CUpwAUSMPWplus_NEMO : public CNEMONumerics { private: diff --git a/SU2_CFD/include/numerics/NEMO/convection/lax.hpp b/SU2_CFD/include/numerics/NEMO/convection/lax.hpp index 520ea76e1e2..d52b4d9ca59 100644 --- a/SU2_CFD/include/numerics/NEMO/convection/lax.hpp +++ b/SU2_CFD/include/numerics/NEMO/convection/lax.hpp @@ -34,7 +34,6 @@ * \brief Class for computing the Lax-Friedrich centered scheme. * \ingroup ConvDiscr * \author F. Palacios, S.R. Copeland, W. Maier, C. Garbacz - * \version 7.0.8 */ class CCentLax_NEMO : public CNEMONumerics { private: diff --git a/SU2_CFD/include/solvers/CSolverFactory.hpp b/SU2_CFD/include/solvers/CSolverFactory.hpp index 6fa7ec0cfa8..1b199c15ca8 100644 --- a/SU2_CFD/include/solvers/CSolverFactory.hpp +++ b/SU2_CFD/include/solvers/CSolverFactory.hpp @@ -2,7 +2,7 @@ * \file CSolverFactory.hpp * \brief Headers of the CSolverFactory class * \author T. Albring - * \version 7.0.1 "Blackbird" + * \version 7.1.1 "Blackbird" * * SU2 Project Website: https://su2code.github.io * diff --git a/SU2_CFD/include/variables/CNEMOEulerVariable.hpp b/SU2_CFD/include/variables/CNEMOEulerVariable.hpp index cf2b0320dc2..f01ff2adf18 100644 --- a/SU2_CFD/include/variables/CNEMOEulerVariable.hpp +++ b/SU2_CFD/include/variables/CNEMOEulerVariable.hpp @@ -35,7 +35,6 @@ * \brief Main class for defining the variables of the NEMO Euler's solver. * \ingroup Euler_Equations * \author S. R. Copeland, F. Palacios, W. Maier, C. Garbacz - * \version 7.0.8 */ class CNEMOEulerVariable : public CVariable { public: diff --git a/SU2_CFD/include/variables/CNEMONSVariable.hpp b/SU2_CFD/include/variables/CNEMONSVariable.hpp index ac9c45f3118..1a4c07e61d3 100644 --- a/SU2_CFD/include/variables/CNEMONSVariable.hpp +++ b/SU2_CFD/include/variables/CNEMONSVariable.hpp @@ -34,7 +34,6 @@ * \brief Main class for defining the variables of the NEMO Navier-Stokes' solver. * \ingroup Navier_Stokes_Equations * \author C. Garbacz, W. Maier, S.R. Copeland. - * \version 7.0.8 */ class CNEMONSVariable final : public CNEMOEulerVariable { private: diff --git a/SU2_CFD/src/output/CNEMOCompOutput.cpp b/SU2_CFD/src/output/CNEMOCompOutput.cpp index b4709a3de6a..7419e311ac2 100644 --- a/SU2_CFD/src/output/CNEMOCompOutput.cpp +++ b/SU2_CFD/src/output/CNEMOCompOutput.cpp @@ -2,7 +2,7 @@ * \file CNEMOCompOutput.cpp * \brief Main subroutines for compressible flow output * \author W. Maier, R. Sanchez - * \version 7.0.0 "Blackbird" + * \version 7.1.1 "Blackbird" * * The current SU2 release has been coordinated by the * SU2 International Developers Society diff --git a/SU2_CFD/src/solvers/CEulerSolver.cpp b/SU2_CFD/src/solvers/CEulerSolver.cpp index ba1a20034e4..19ee3038c6f 100644 --- a/SU2_CFD/src/solvers/CEulerSolver.cpp +++ b/SU2_CFD/src/solvers/CEulerSolver.cpp @@ -8567,7 +8567,6 @@ void CEulerSolver::BC_ActDisk_VariableLoad(CGeometry *geometry, CSolver **solver * \brief Actuator disk model with variable load along disk radius. * \author: E. Saetta, L. Russo, R. Tognaccini (GitHub references EttoreSaetta, lorenzorusso07, rtogna). * Theoretical and Applied Aerodynamics Research Group (TAARG), University of Naples Federico II. - * \version 7.0.6 “Blackbird” * First release date : July 1st 2020 * modified on: * diff --git a/SU2_PY/convert_to_csv.py b/SU2_PY/convert_to_csv.py index a5c6994acf8..c8fd823333d 100755 --- a/SU2_PY/convert_to_csv.py +++ b/SU2_PY/convert_to_csv.py @@ -3,7 +3,7 @@ ## \file convert_to_csv.py # \brief This script converts SU2 ASCII restart files generated with a version prior v7 to the CSV format # \author T. Albring -# \version 7.0.0 "Falcon" +# \version 7.1.1 "Blackbird" # # SU2 Project Website: https://su2code.github.io # diff --git a/SU2_PY/pySU2/pySU2ad.i b/SU2_PY/pySU2/pySU2ad.i index d873a96aaa4..aaf37844c90 100644 --- a/SU2_PY/pySU2/pySU2ad.i +++ b/SU2_PY/pySU2/pySU2ad.i @@ -4,7 +4,7 @@ # \file pySU2ad.i # \brief Configuration file for the Swig compilation of the Python wrapper. # \author D. Thomas, R. Sanchez -# \version 7.0.0 "Falcon" +# \version 7.1.1 "Blackbird" # # SU2 Project Website: https://su2code.github.io # diff --git a/SU2_PY/updateHistoryMap.py b/SU2_PY/updateHistoryMap.py index 8b3681df716..f69df1d4aec 100644 --- a/SU2_PY/updateHistoryMap.py +++ b/SU2_PY/updateHistoryMap.py @@ -3,7 +3,7 @@ ## \file updateHistoryMap.py # \brief Python script for updating the historyMap.py file. # \author T. Albring -# \version 7.0.0 "Falcon" +# \version 7.1.1 "Blackbird" # # SU2 Project Website: https://su2code.github.io # diff --git a/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg index 5377b2c322a..1f69a0559ae 100644 --- a/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg +++ b/TestCases/coupled_cht/comp_2d/cht_2d_3cylinders.cfg @@ -5,7 +5,7 @@ % Author: O. Burghardt % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: January 6, 2020 % -% File Version 7.0 "Blackbird" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg index 51f91e81539..a4402f99503 100644 --- a/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg +++ b/TestCases/coupled_cht/disc_adj_incomp_2d/cht_2d_3cylinders.cfg @@ -5,7 +5,7 @@ % Author: O. Burghardt, T. Economon % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: August 8, 2019 % -% File Version 6.0.1 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg index d0804e33899..e8c3ceaced6 100644 --- a/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg +++ b/TestCases/coupled_cht/incomp_2d/cht_2d_3cylinders.cfg @@ -5,7 +5,7 @@ % Author: O. Burghardt, T. Economon % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: August 8, 2019 % -% File Version 6.0.1 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg b/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg index 249e9928a84..9689ff4bb6b 100644 --- a/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg +++ b/TestCases/coupled_cht/incomp_2d_unsteady/cht_2d_3cylinders.cfg @@ -5,7 +5,7 @@ % Author: O. Burghardt, T. Economon % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: August 8, 2019 % -% File Version 6.0.1 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/deformation/intersection_prevention/def_intersect.cfg b/TestCases/deformation/intersection_prevention/def_intersect.cfg index 5a934a6e1cb..2a4417eee95 100644 --- a/TestCases/deformation/intersection_prevention/def_intersect.cfg +++ b/TestCases/deformation/intersection_prevention/def_intersect.cfg @@ -15,7 +15,7 @@ % Institution: % % Technische Universiteit Eindhoven % % Date: 2021.01.08 % -% File Version 7.0.8 "Blackbird" % +% File Version 7.1.1 "Blackbird" % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------% diff --git a/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg b/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg index aa2f40ef719..83c62c096c1 100644 --- a/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg +++ b/TestCases/disc_adj_euler/arina2k/Arina2KRS.cfg @@ -6,7 +6,7 @@ % Author: Jairo Paes Cavalcante Filho [Based on T. Economon & M. Pini work] % % Institution: University of São Paulo % % Date: 8-JUL-2018 % -% File Version 6.1.0 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/disc_adj_rans/cylinder/cylinder.cfg b/TestCases/disc_adj_rans/cylinder/cylinder.cfg index eb008d5a254..d0c809d304a 100644 --- a/TestCases/disc_adj_rans/cylinder/cylinder.cfg +++ b/TestCases/disc_adj_rans/cylinder/cylinder.cfg @@ -2,10 +2,10 @@ % % % SU2 configuration file % % Case description: Turbulent unsteady flow around a cylinder % -% Author: Tim Albring % +% Author: Tim Albring % % Institution: TU Kaiserslautern % % Date: 2016.06.14 % -% File Version 4.2 "Cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg index 8243441ad17..68b805ef643 100644 --- a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg +++ b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg @@ -2,10 +2,10 @@ % % % SU2 configuration file % % Case description: Turbulent unsteady flow around a cylinder % -% Author: Tim Albring % +% Author: Tim Albring % % Institution: TU Kaiserslautern % % Date: 2016.06.14 % -% File Version 4.2 "Cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg index ac050e34e4f..e1242e2f903 100644 --- a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg +++ b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg @@ -2,10 +2,10 @@ % % % SU2 configuration file % % Case description: Turbulent unsteady flow around a cylinder % -% Author: Tim Albring % +% Author: Tim Albring % % Institution: TU Kaiserslautern % % Date: 2016.06.14 % -% File Version 4.2 "Cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg b/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg index 910f4f8e97d..0c8985c975d 100644 --- a/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg +++ b/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg @@ -2,10 +2,10 @@ % % % SU2 configuration file % % Case description: Turbulent unsteady flow around a cylinder % -% Author: Tim Albring % +% Author: Tim Albring % % Institution: TU Kaiserslautern % % Date: 2016.06.14 % -% File Version 4.2 "Cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg index a6fa41a303e..340f2bd202e 100644 --- a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg +++ b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sa.cfg @@ -3,10 +3,10 @@ % SU2 configuration file % % Case description: 2D NACA 0012 Airfoil Validation Case (compressible) % % http://turbmodels.larc.nasa.gov/naca0012_val_sa.html % -% Author: Francisco Palacios % +% Author: Francisco Palacios % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg index 219c40f6639..07f2247774a 100644 --- a/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg +++ b/TestCases/disc_adj_rans/naca0012/turb_NACA0012_sst.cfg @@ -6,7 +6,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg index 79d6f2319ee..d6968df5ce3 100644 --- a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg +++ b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg @@ -1,11 +1,11 @@ %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % % % SU2 configuration file % -% Case description: Transonic ORC nozzle % +% Case description: Transonic ORC nozzle % % Author: S. Vitale % % Institution: Delft University of Technology % % Date: 2017.03.01 % -% File Version 5.0.0 "Cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/euler/bluntbody/blunt.cfg b/TestCases/euler/bluntbody/blunt.cfg index 1e0a66b9b43..71e413f80a0 100644 --- a/TestCases/euler/bluntbody/blunt.cfg +++ b/TestCases/euler/bluntbody/blunt.cfg @@ -5,7 +5,7 @@ % Author: Amit Sachdeva % % Institution: ADSG-VSSC % % Date: 2019.01.23 % -% File Version 6.1.0 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/fea_fsi/Airfoil_RBF/config.cfg b/TestCases/fea_fsi/Airfoil_RBF/config.cfg index ddcf42c9b8e..985f7ffb0ff 100755 --- a/TestCases/fea_fsi/Airfoil_RBF/config.cfg +++ b/TestCases/fea_fsi/Airfoil_RBF/config.cfg @@ -3,7 +3,7 @@ % Case description: 2D airfoil FSI with radial basis function interp. % % Institution: Imperial College London % % Date: 2015.08.12 % -% File Version 7.0.2 "Blackbird" % +% File Version 7.1.1 "Blackbird" % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% SOLVER = MULTIPHYSICS diff --git a/TestCases/fea_fsi/SquareCyl_Beam/config.cfg b/TestCases/fea_fsi/SquareCyl_Beam/config.cfg index 311b9687653..cf42dd47862 100644 --- a/TestCases/fea_fsi/SquareCyl_Beam/config.cfg +++ b/TestCases/fea_fsi/SquareCyl_Beam/config.cfg @@ -5,7 +5,7 @@ % Author: Ruben Sanchez Fernandez % % Institution: Imperial College London % % Date: 2016.06.01 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg b/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg index 1b662bdc67a..a4a362e1e00 100644 --- a/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg +++ b/TestCases/fixed_cl/naca0012/inv_NACA0012.cfg @@ -5,7 +5,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: 2014.06.11 % -% File Version 3.2.8 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg b/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg index 4bcea99b789..1275f84336f 100644 --- a/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg +++ b/TestCases/fixed_cl/naca0012/inv_NACA0012_ContAdj.cfg @@ -5,7 +5,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: 2014.06.11 % -% File Version 3.2.8 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configFluid.cfg b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configFluid.cfg index 2cf3958cda3..ba44689335e 100644 --- a/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configFluid.cfg +++ b/TestCases/incomp_navierstokes/streamwise_periodic/chtPinArray_2d/configFluid.cfg @@ -5,7 +5,7 @@ % Author: T. Kattmann % % Institution: Robert Bosch GmbH % % Date: 2020.12.15 % -% File Version 7.0.8 "Blackbird" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg b/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg index 906d02008bc..664db52e5ec 100644 --- a/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg +++ b/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg @@ -5,7 +5,7 @@ % pressure gradient % % Author: Akshay Koodly % % Date: 2020.07.07 % -% File Version 7.0.x "Blackbird" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/mms/dg_ringleb/ringleb_dg.cfg b/TestCases/mms/dg_ringleb/ringleb_dg.cfg index 81a40814dfc..ae5111d971e 100644 --- a/TestCases/mms/dg_ringleb/ringleb_dg.cfg +++ b/TestCases/mms/dg_ringleb/ringleb_dg.cfg @@ -5,7 +5,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: 2014.06.11 % -% File Version 4.0.2 "Cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg b/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg index 9f3aa142194..619638f88cf 100644 --- a/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg +++ b/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg @@ -2,10 +2,10 @@ % % % SU2 configuration file % % Case description: Poiseuille flow case for testing inlet profile files % -% Author: Thomas D. Economon % +% Author: Thomas D. Economon % % Institution: Robert Bosch LLC % % Date: 2018.03.19 % -% File Version 6.0.0 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/nicf/LS89/turb_SA_PR.cfg b/TestCases/nicf/LS89/turb_SA_PR.cfg index 7c1fa4fe5d6..525a0c2a83a 100644 --- a/TestCases/nicf/LS89/turb_SA_PR.cfg +++ b/TestCases/nicf/LS89/turb_SA_PR.cfg @@ -5,7 +5,7 @@ % Author: M. Pini, S. Vitale % % Institution: Delft University of Technology % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/nicf/LS89/turb_SST_PR.cfg b/TestCases/nicf/LS89/turb_SST_PR.cfg index 6f41a50d4a8..d5b6aa40938 100644 --- a/TestCases/nicf/LS89/turb_SST_PR.cfg +++ b/TestCases/nicf/LS89/turb_SST_PR.cfg @@ -5,7 +5,7 @@ % Author: M. Pini, S. Vitale % % Institution: Delft University of Technology % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg b/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg index bb61cbdf1ab..5a7fd3d389d 100644 --- a/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg +++ b/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg @@ -4,10 +4,10 @@ % Case description: 2D 5x5 Square Test Case representing a thermal bath % % with thermal nonequilibrium and finite-rate chemistry % % % -% Author: C. Garbacz % +% Author: C. Garbacz % % Institution: Strathclyde University % % Date: 2019.04.10 % -% File Version 7.0.6 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg b/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg index 8ddd0b7fd3a..8a46ede2a28 100644 --- a/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg +++ b/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg @@ -6,7 +6,7 @@ % Author: C. Garbacz % % Institution: Strathclyde University % % Date: 2019.04.10 % -% File Version 7.0.6 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg index d24de29bff2..c6b69b57b33 100644 --- a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg +++ b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg @@ -5,7 +5,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: 2014.06.11 % -% File Version 3.2.7 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/rans/naca0012/turb_NACA0012_sa.cfg b/TestCases/rans/naca0012/turb_NACA0012_sa.cfg index 2191db91136..46d95de0243 100644 --- a/TestCases/rans/naca0012/turb_NACA0012_sa.cfg +++ b/TestCases/rans/naca0012/turb_NACA0012_sa.cfg @@ -3,10 +3,10 @@ % SU2 configuration file % % Case description: 2D NACA 0012 Airfoil Validation Case (compressible) % % http://turbmodels.larc.nasa.gov/naca0012_val_sa.html % -% Author: Francisco Palacios % +% Author: Francisco Palacios % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/rans/naca0012/turb_NACA0012_sa_binary.cfg b/TestCases/rans/naca0012/turb_NACA0012_sa_binary.cfg index 81cfe385e56..b579467180c 100644 --- a/TestCases/rans/naca0012/turb_NACA0012_sa_binary.cfg +++ b/TestCases/rans/naca0012/turb_NACA0012_sa_binary.cfg @@ -3,10 +3,10 @@ % SU2 configuration file % % Case description: 2D NACA 0012 Airfoil Validation Case (compressible) % % http://turbmodels.larc.nasa.gov/naca0012_val_sa.html % -% Author: Francisco Palacios % +% Author: Francisco Palacios % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/rans/naca0012/turb_NACA0012_sa_neg.cfg b/TestCases/rans/naca0012/turb_NACA0012_sa_neg.cfg index c7777fcbf39..2a84ec66f3a 100644 --- a/TestCases/rans/naca0012/turb_NACA0012_sa_neg.cfg +++ b/TestCases/rans/naca0012/turb_NACA0012_sa_neg.cfg @@ -3,10 +3,10 @@ % SU2 configuration file % % Case description: 2D NACA 0012 Airfoil Validation Case (compressible) % % http://turbmodels.larc.nasa.gov/naca0012_val_sa.html % -% Author: Francisco Palacios % +% Author: Francisco Palacios % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst.cfg index ccabc3bdd5f..7ec8feefc67 100644 --- a/TestCases/rans/naca0012/turb_NACA0012_sst.cfg +++ b/TestCases/rans/naca0012/turb_NACA0012_sst.cfg @@ -6,7 +6,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg b/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg index 256a6cf02a0..3dec2f00ecd 100644 --- a/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg +++ b/TestCases/rans/naca0012/turb_NACA0012_sst_sust.cfg @@ -6,7 +6,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg index 7a544fec73e..6c6d15b3b20 100644 --- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg +++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq.cfg @@ -6,7 +6,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg index 394791d5d9a..c5bbedb075d 100644 --- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg +++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_1c.cfg @@ -6,7 +6,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg index 1a2bbe9883f..32f4881e58a 100644 --- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg +++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_2c.cfg @@ -6,7 +6,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg index fd9d8d96c7f..9f71746476e 100644 --- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg +++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_3c.cfg @@ -6,7 +6,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg index b8b89ac9611..a83e57b0932 100644 --- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg +++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c1.cfg @@ -6,7 +6,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg index 31880344bb4..e04a67be9bd 100644 --- a/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg +++ b/TestCases/rans_uq/naca0012/turb_NACA0012_uq_p1c2.cfg @@ -6,7 +6,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: Feb 18th, 2013 % -% File Version 3.2.1 "eagle" % +% File Version 7.1.1 "Blackbird % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg b/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg index f0a679bbd43..f13f54b3792 100644 --- a/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg +++ b/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg @@ -4,9 +4,9 @@ % Case description: 2D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg b/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg index 1686b4f7d76..3b6183fd7c3 100644 --- a/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg +++ b/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg @@ -4,9 +4,9 @@ % Case description: 2D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg b/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg index 2f27f2f4d8b..ded31611626 100644 --- a/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg +++ b/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg b/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg index 38594f853df..f8101410074 100644 --- a/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg +++ b/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/channel_3D/zone_1.cfg b/TestCases/sliding_interface/channel_3D/zone_1.cfg index a1f382bb16d..b8f197a033b 100644 --- a/TestCases/sliding_interface/channel_3D/zone_1.cfg +++ b/TestCases/sliding_interface/channel_3D/zone_1.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/channel_3D/zone_2.cfg b/TestCases/sliding_interface/channel_3D/zone_2.cfg index ec1aa76bc15..937a5b0a5f5 100644 --- a/TestCases/sliding_interface/channel_3D/zone_2.cfg +++ b/TestCases/sliding_interface/channel_3D/zone_2.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % ----------------------- DYNAMIC MESH DEFINITION -----------------------------% diff --git a/TestCases/sliding_interface/channel_3D/zone_3.cfg b/TestCases/sliding_interface/channel_3D/zone_3.cfg index 59c20711a6d..0e42d310305 100644 --- a/TestCases/sliding_interface/channel_3D/zone_3.cfg +++ b/TestCases/sliding_interface/channel_3D/zone_3.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % ----------------------- DYNAMIC MESH DEFINITION -----------------------------% diff --git a/TestCases/sliding_interface/incompressible_steady/config.cfg b/TestCases/sliding_interface/incompressible_steady/config.cfg index cfc7414fa7d..a6631a16a43 100644 --- a/TestCases/sliding_interface/incompressible_steady/config.cfg +++ b/TestCases/sliding_interface/incompressible_steady/config.cfg @@ -5,7 +5,7 @@ % Author: Ruben Sanchez % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: January 28th, 2018 % -% File Version 6.1.0 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/incompressible_steady/configCircle.cfg b/TestCases/sliding_interface/incompressible_steady/configCircle.cfg index 16b4df86d65..e3e30763507 100644 --- a/TestCases/sliding_interface/incompressible_steady/configCircle.cfg +++ b/TestCases/sliding_interface/incompressible_steady/configCircle.cfg @@ -5,7 +5,7 @@ % Author: Ruben Sanchez % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: January 28th, 2018 % -% File Version 6.1.0 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/incompressible_steady/configOut.cfg b/TestCases/sliding_interface/incompressible_steady/configOut.cfg index 9e42a671236..97ad384eaab 100644 --- a/TestCases/sliding_interface/incompressible_steady/configOut.cfg +++ b/TestCases/sliding_interface/incompressible_steady/configOut.cfg @@ -5,7 +5,7 @@ % Author: Ruben Sanchez % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: January 28th, 2018 % -% File Version 6.1.0 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/incompressible_unsteady/config.cfg b/TestCases/sliding_interface/incompressible_unsteady/config.cfg index 81a7c8bbf02..2bbbbb98c8a 100644 --- a/TestCases/sliding_interface/incompressible_unsteady/config.cfg +++ b/TestCases/sliding_interface/incompressible_unsteady/config.cfg @@ -5,7 +5,7 @@ % Author: Ruben Sanchez % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: January 28th, 2018 % -% File Version 6.1.0 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg b/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg index 4082db97ddf..a196ffdea01 100644 --- a/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg +++ b/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg @@ -5,7 +5,7 @@ % Author: Ruben Sanchez % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: January 28th, 2018 % -% File Version 6.1.0 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg b/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg index c104e40ec79..be56fac04c1 100644 --- a/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg +++ b/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg @@ -5,7 +5,7 @@ % Author: Ruben Sanchez % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: January 28th, 2018 % -% File Version 6.1.0 "Falcon" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/pipe/pipe_NN.cfg b/TestCases/sliding_interface/pipe/pipe_NN.cfg index 9814d9a8152..d4c4c4d14ac 100644 --- a/TestCases/sliding_interface/pipe/pipe_NN.cfg +++ b/TestCases/sliding_interface/pipe/pipe_NN.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/pipe/pipe_WA.cfg b/TestCases/sliding_interface/pipe/pipe_WA.cfg index c59374a4b67..8ad225ba535 100644 --- a/TestCases/sliding_interface/pipe/pipe_WA.cfg +++ b/TestCases/sliding_interface/pipe/pipe_WA.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/pipe/zone_1.cfg b/TestCases/sliding_interface/pipe/zone_1.cfg index 827e224c8d7..f238407ffaf 100644 --- a/TestCases/sliding_interface/pipe/zone_1.cfg +++ b/TestCases/sliding_interface/pipe/zone_1.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/pipe/zone_2.cfg b/TestCases/sliding_interface/pipe/zone_2.cfg index 356ae57f46e..7e30feded3a 100644 --- a/TestCases/sliding_interface/pipe/zone_2.cfg +++ b/TestCases/sliding_interface/pipe/zone_2.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/pipe/zone_3.cfg b/TestCases/sliding_interface/pipe/zone_3.cfg index 79c7b428c38..e70627cbf24 100644 --- a/TestCases/sliding_interface/pipe/zone_3.cfg +++ b/TestCases/sliding_interface/pipe/zone_3.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/pipe/zone_4.cfg b/TestCases/sliding_interface/pipe/zone_4.cfg index 2604ae779f5..0b7d28345f6 100644 --- a/TestCases/sliding_interface/pipe/zone_4.cfg +++ b/TestCases/sliding_interface/pipe/zone_4.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/pipe/zone_5.cfg b/TestCases/sliding_interface/pipe/zone_5.cfg index be99c6a8d1e..e6db5eecea9 100644 --- a/TestCases/sliding_interface/pipe/zone_5.cfg +++ b/TestCases/sliding_interface/pipe/zone_5.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg index 6978fb60251..c44185acc4e 100644 --- a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg +++ b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg @@ -3,9 +3,9 @@ % SU2 configuration file % % Case description: 2D, four cylynders rotating inside a supersonic flow % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg index 88b93d6a4c4..551dc1745e7 100644 --- a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg +++ b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg @@ -3,9 +3,9 @@ % SU2 configuration file % % Case description: 2D, four cylynders rotating inside a supersonic flow % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/single_stage/single_stage_NN.cfg b/TestCases/sliding_interface/single_stage/single_stage_NN.cfg index af408c66940..6ada93b0aae 100644 --- a/TestCases/sliding_interface/single_stage/single_stage_NN.cfg +++ b/TestCases/sliding_interface/single_stage/single_stage_NN.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/single_stage/single_stage_WA.cfg b/TestCases/sliding_interface/single_stage/single_stage_WA.cfg index 85d46c8bb50..c5a70f92f26 100644 --- a/TestCases/sliding_interface/single_stage/single_stage_WA.cfg +++ b/TestCases/sliding_interface/single_stage/single_stage_WA.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/single_stage/zone_1.cfg b/TestCases/sliding_interface/single_stage/zone_1.cfg index 9e2f232e2b3..cfbcf1afde0 100644 --- a/TestCases/sliding_interface/single_stage/zone_1.cfg +++ b/TestCases/sliding_interface/single_stage/zone_1.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/single_stage/zone_2.cfg b/TestCases/sliding_interface/single_stage/zone_2.cfg index 136ffadfaff..c35971a3b23 100644 --- a/TestCases/sliding_interface/single_stage/zone_2.cfg +++ b/TestCases/sliding_interface/single_stage/zone_2.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg index 7c162900718..6ebd99563ec 100644 --- a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg +++ b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg @@ -4,9 +4,9 @@ % Case description: 2D inviscid, this test case reproduces vortex shedding % % after a cylindrical body in a supersonic upstream flow % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg index 02d5f916fed..4c53e46103d 100644 --- a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg +++ b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg @@ -4,9 +4,9 @@ % Case description: 2D inviscid, this test case reproduces vortex shedding % % after a cylindrical body in a supersonic upstream flow % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg index b362d5479e2..dd85801b80d 100644 --- a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg +++ b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg @@ -4,9 +4,9 @@ % Case description: 2D inviscid, this test case reproduces vortex shedding % % after a cylindrical body in a supersonic upstream flow % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % ----------------------- DYNAMIC MESH DEFINITION -----------------------------% diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg index d14c032f9e6..bcd85355708 100644 --- a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg +++ b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg @@ -4,9 +4,9 @@ % Case description: 2D inviscid, this test case reproduces vortex shedding % % after a cylindrical body in a supersonic upstream flow % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % ----------------------- DYNAMIC MESH DEFINITION -----------------------------% diff --git a/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg b/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg index 507b75beb92..34f7b0f7613 100644 --- a/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg +++ b/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg @@ -4,9 +4,9 @@ % Case description: 2D, inviscid flow, this test case is used for debugging % % purposes, part of the grid is moving % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg b/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg index 5ea9fc4819d..492db3a2cf3 100644 --- a/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg +++ b/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg @@ -4,9 +4,9 @@ % Case description: 2D, inviscid flow, this test case is used for debugging % % purposes, part of the grid is moving % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/uniform_flow/zone_1.cfg b/TestCases/sliding_interface/uniform_flow/zone_1.cfg index 05721da54b9..399bdc2f868 100644 --- a/TestCases/sliding_interface/uniform_flow/zone_1.cfg +++ b/TestCases/sliding_interface/uniform_flow/zone_1.cfg @@ -4,9 +4,9 @@ % Case description: 2D, inviscid flow, this test case is used for debugging % % purposes, part of the grid is moving % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % ----------------------- DYNAMIC MESH DEFINITION -----------------------------% diff --git a/TestCases/sliding_interface/uniform_flow/zone_2.cfg b/TestCases/sliding_interface/uniform_flow/zone_2.cfg index ddd50c65a42..b1c64f70a42 100644 --- a/TestCases/sliding_interface/uniform_flow/zone_2.cfg +++ b/TestCases/sliding_interface/uniform_flow/zone_2.cfg @@ -4,9 +4,9 @@ % Case description: 2D, inviscid flow, this test case is used for debugging % % purposes, part of the grid is moving % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 4.3.0 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % ----------------------- DYNAMIC MESH DEFINITION -----------------------------% diff --git a/TestCases/turbomachinery/APU_turbocharger/Jones.cfg b/TestCases/turbomachinery/APU_turbocharger/Jones.cfg index 7e30abe447d..746f5bfbf1b 100755 --- a/TestCases/turbomachinery/APU_turbocharger/Jones.cfg +++ b/TestCases/turbomachinery/APU_turbocharger/Jones.cfg @@ -5,7 +5,7 @@ % Author: S. Vitale % % Institution: Delft University of Technology % % Date: Jun 28th, 2017 % -% File Version 5.0.0"cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/turbomachinery/APU_turbocharger/Jones_rst.cfg b/TestCases/turbomachinery/APU_turbocharger/Jones_rst.cfg index 333c460f3ed..a8a95f2ec12 100755 --- a/TestCases/turbomachinery/APU_turbocharger/Jones_rst.cfg +++ b/TestCases/turbomachinery/APU_turbocharger/Jones_rst.cfg @@ -5,7 +5,7 @@ % Author: S. Vitale % % Institution: Delft University of Technology % % Date: Jun 28th, 2017 % -% File Version 5.0.0"cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg b/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg index 278775aa873..3ecdef0cab6 100755 --- a/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg +++ b/TestCases/turbomachinery/axial_stage_2D/Axial_stage2D.cfg @@ -5,7 +5,7 @@ % Author: S. Vitale % % Institution: Delft University of Technology % % Date: Feb 28th, 2017 % -% File Version 5.0.0"cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/turbomachinery/axial_stage_2D/zone_1.cfg b/TestCases/turbomachinery/axial_stage_2D/zone_1.cfg index 3ddcc043834..80c260bb0cd 100644 --- a/TestCases/turbomachinery/axial_stage_2D/zone_1.cfg +++ b/TestCases/turbomachinery/axial_stage_2D/zone_1.cfg @@ -5,7 +5,7 @@ % Author: S. Vitale % % Institution: Delft University of Technology % % Date: Feb 28th, 2017 % -% File Version 5.0.0"cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/turbomachinery/axial_stage_2D/zone_2.cfg b/TestCases/turbomachinery/axial_stage_2D/zone_2.cfg index 02acc04d938..eeeedce3611 100644 --- a/TestCases/turbomachinery/axial_stage_2D/zone_2.cfg +++ b/TestCases/turbomachinery/axial_stage_2D/zone_2.cfg @@ -5,7 +5,7 @@ % Author: S. Vitale % % Institution: Delft University of Technology % % Date: Feb 28th, 2017 % -% File Version 5.0.0"cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg b/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg index 140c6d8dfa1..119320318e3 100755 --- a/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg +++ b/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg @@ -2,10 +2,10 @@ % % % SU2 configuration file % % Case description: Centrifugal turbine rotor % -% Author:S. Vitale % +% Author:S. Vitale % % Institution: Delft University of Technology % % Date: Oct 26th, 2015 % -% File Version 4.0.1 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg b/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg index 69740ee71b8..7031b42b19d 100755 --- a/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg +++ b/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg @@ -5,7 +5,7 @@ % Author: S. Vitale % % Institution: Delft University of Technology % % Date: Oct 28th, 2015 % -% File Version 4.0.1 "cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator.cfg b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator.cfg index 25d1cb0b3a2..42f76d6afd0 100644 --- a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator.cfg +++ b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator.cfg @@ -1,11 +1,11 @@ %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % % % SU2 configuration file % -% Case description: Transonic ORC nozzle % +% Case description: Transonic ORC nozzle % % Author: S. Vitale % % Institution: Delft University of Technology % % Date: 2017.03.01 % -% File Version 5.0.0 "Cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_rst.cfg b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_rst.cfg index eded8208271..48778dcf05f 100644 --- a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_rst.cfg +++ b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator_rst.cfg @@ -1,11 +1,11 @@ %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % % % SU2 configuration file % -% Case description: Transonic ORC nozzle % +% Case description: Transonic ORC nozzle % % Author: S. Vitale % % Institution: Delft University of Technology % % Date: 2017.03.01 % -% File Version 5.0.0 "Cardinal" % +% File Version 7.1.1 "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/configure.ac b/configure.ac index dc9ac9b6e32..726da250fa4 100644 --- a/configure.ac +++ b/configure.ac @@ -338,7 +338,7 @@ AC_MSG_RESULT([ ------------------------------------------------------------------------- | ___ _ _ ___ | -| / __| | | |_ ) Release 6.2.0 'Falcon' | +| / __| | | |_ ) Release 7.1.1 'Blackbird' | | \\__ \\ |_| |/ / | | |___/\\___//___| Suite | | | diff --git a/externals/tecio/Makefile.am b/externals/tecio/Makefile.am index 28504fce90e..bbdf397afa5 100644 --- a/externals/tecio/Makefile.am +++ b/externals/tecio/Makefile.am @@ -3,7 +3,7 @@ # \file Makefile.am # \brief Makefile for external libraries # \author B. Kirk, T. Economon, F. Palacios -# \version 6.1.0 "Falcon" +# \version 7.1.1 "Blackbird" # # The current SU2 release has been coordinated by the # SU2 International Developers Society From 1882b644c397c0a45b3d51657897ce5c08c1066a Mon Sep 17 00:00:00 2001 From: WallyMaier Date: Tue, 27 Apr 2021 14:39:42 -0700 Subject: [PATCH 2/2] Removing tabs, reverting some changes due to unknown uses --- TestCases/disc_adj_rans/cylinder/cylinder.cfg | 2 +- .../cylinder/cylinder_Windowing.cfg | 2 +- .../cylinder/cylinder_Windowing_AD.cfg | 2 +- .../cylinder_DT_1ST/cylinder.cfg | 2 +- .../transonic_stator_2D/transonic_stator.cfg | 2 +- TestCases/fea_fsi/SquareCyl_Beam/config.cfg | 2 +- .../rough_flatplate_incomp.cfg | 2 +- .../poiseuille/profile_poiseuille.cfg | 2 +- .../finitechemistry/thermalbath.cfg | 2 +- .../thermalbath/frozen/thermalbath_frozen.cfg | 2 +- .../steady_inverse_design/inv_NACA0012.cfg | 2 +- TestCases/rans/naca0012/turb_NACA0012_sa.cfg | 2 +- .../rans/naca0012/turb_NACA0012_sa_binary.cfg | 252 ------------------ .../rans/naca0012/turb_NACA0012_sa_neg.cfg | 239 ----------------- .../channel_2D/channel_2D_NN.cfg | 2 +- .../channel_2D/channel_2D_WA.cfg | 2 +- .../channel_3D/channel_3D_NN.cfg | 2 +- .../channel_3D/channel_3D_WA.cfg | 2 +- .../sliding_interface/channel_3D/zone_1.cfg | 2 +- .../sliding_interface/channel_3D/zone_2.cfg | 2 +- .../sliding_interface/channel_3D/zone_3.cfg | 2 +- .../incompressible_unsteady/config.cfg | 2 +- .../incompressible_unsteady/configCircle.cfg | 2 +- .../incompressible_unsteady/configOut.cfg | 2 +- TestCases/sliding_interface/pipe/pipe_NN.cfg | 2 +- TestCases/sliding_interface/pipe/pipe_WA.cfg | 2 +- TestCases/sliding_interface/pipe/zone_1.cfg | 2 +- TestCases/sliding_interface/pipe/zone_2.cfg | 2 +- TestCases/sliding_interface/pipe/zone_3.cfg | 2 +- TestCases/sliding_interface/pipe/zone_4.cfg | 2 +- TestCases/sliding_interface/pipe/zone_5.cfg | 2 +- .../rotating_cylinders/rot_cylinders_NN.cfg | 2 +- .../rotating_cylinders/rot_cylinders_WA.cfg | 2 +- .../single_stage/single_stage_NN.cfg | 4 +- .../single_stage/single_stage_WA.cfg | 4 +- .../sliding_interface/single_stage/zone_1.cfg | 4 +- .../sliding_interface/single_stage/zone_2.cfg | 4 +- .../sup_vor_shed_NN.cfg | 2 +- .../sup_vor_shed_WA.cfg | 2 +- .../supersonic_vortex_shedding/zone_1.cfg | 2 +- .../supersonic_vortex_shedding/zone_2.cfg | 2 +- .../uniform_flow/uniform_NN.cfg | 2 +- .../uniform_flow/uniform_WA.cfg | 2 +- .../sliding_interface/uniform_flow/zone_1.cfg | 2 +- .../sliding_interface/uniform_flow/zone_2.cfg | 2 +- .../centrifugal_blade/centrifugal_blade.cfg | 4 +- .../centrifugal_stage/centrifugal_stage.cfg | 2 +- .../transonic_stator_2D/transonic_stator.cfg | 2 +- 48 files changed, 51 insertions(+), 542 deletions(-) delete mode 100644 TestCases/rans/naca0012/turb_NACA0012_sa_binary.cfg delete mode 100644 TestCases/rans/naca0012/turb_NACA0012_sa_neg.cfg diff --git a/TestCases/disc_adj_rans/cylinder/cylinder.cfg b/TestCases/disc_adj_rans/cylinder/cylinder.cfg index d0c809d304a..551a53faa96 100644 --- a/TestCases/disc_adj_rans/cylinder/cylinder.cfg +++ b/TestCases/disc_adj_rans/cylinder/cylinder.cfg @@ -2,7 +2,7 @@ % % % SU2 configuration file % % Case description: Turbulent unsteady flow around a cylinder % -% Author: Tim Albring % +% Author: Tim Albring % % Institution: TU Kaiserslautern % % Date: 2016.06.14 % % File Version 7.1.1 "Blackbird" % diff --git a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg index 68b805ef643..37d598dc080 100644 --- a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg +++ b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing.cfg @@ -2,7 +2,7 @@ % % % SU2 configuration file % % Case description: Turbulent unsteady flow around a cylinder % -% Author: Tim Albring % +% Author: Tim Albring % % Institution: TU Kaiserslautern % % Date: 2016.06.14 % % File Version 7.1.1 "Blackbird" % diff --git a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg index e1242e2f903..36884547ad0 100644 --- a/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg +++ b/TestCases/disc_adj_rans/cylinder/cylinder_Windowing_AD.cfg @@ -2,7 +2,7 @@ % % % SU2 configuration file % % Case description: Turbulent unsteady flow around a cylinder % -% Author: Tim Albring % +% Author: Tim Albring % % Institution: TU Kaiserslautern % % Date: 2016.06.14 % % File Version 7.1.1 "Blackbird" % diff --git a/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg b/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg index 0c8985c975d..272929a71b8 100644 --- a/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg +++ b/TestCases/disc_adj_rans/cylinder_DT_1ST/cylinder.cfg @@ -2,7 +2,7 @@ % % % SU2 configuration file % % Case description: Turbulent unsteady flow around a cylinder % -% Author: Tim Albring % +% Author: Tim Albring % % Institution: TU Kaiserslautern % % Date: 2016.06.14 % % File Version 7.1.1 "Blackbird" % diff --git a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg index d6968df5ce3..6256ee7923f 100644 --- a/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg +++ b/TestCases/disc_adj_turbomachinery/transonic_stator_2D/transonic_stator.cfg @@ -1,7 +1,7 @@ %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % % % SU2 configuration file % -% Case description: Transonic ORC nozzle % +% Case description: Transonic ORC nozzle % % Author: S. Vitale % % Institution: Delft University of Technology % % Date: 2017.03.01 % diff --git a/TestCases/fea_fsi/SquareCyl_Beam/config.cfg b/TestCases/fea_fsi/SquareCyl_Beam/config.cfg index cf42dd47862..311b9687653 100644 --- a/TestCases/fea_fsi/SquareCyl_Beam/config.cfg +++ b/TestCases/fea_fsi/SquareCyl_Beam/config.cfg @@ -5,7 +5,7 @@ % Author: Ruben Sanchez Fernandez % % Institution: Imperial College London % % Date: 2016.06.01 % -% File Version 7.1.1 "Blackbird" % +% File Version 4.3.0 "cardinal" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg b/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg index 664db52e5ec..906d02008bc 100644 --- a/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg +++ b/TestCases/incomp_rans/rough_flatplate/rough_flatplate_incomp.cfg @@ -5,7 +5,7 @@ % pressure gradient % % Author: Akshay Koodly % % Date: 2020.07.07 % -% File Version 7.1.1 "Blackbird" % +% File Version 7.0.x "Blackbird" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg b/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg index 619638f88cf..2facd7569d7 100644 --- a/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg +++ b/TestCases/navierstokes/poiseuille/profile_poiseuille.cfg @@ -2,7 +2,7 @@ % % % SU2 configuration file % % Case description: Poiseuille flow case for testing inlet profile files % -% Author: Thomas D. Economon % +% Author: Thomas D. Economon % % Institution: Robert Bosch LLC % % Date: 2018.03.19 % % File Version 7.1.1 "Blackbird" % diff --git a/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg b/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg index 5a7fd3d389d..6ab25c0232b 100644 --- a/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg +++ b/TestCases/nonequilibrium/thermalbath/finitechemistry/thermalbath.cfg @@ -4,7 +4,7 @@ % Case description: 2D 5x5 Square Test Case representing a thermal bath % % with thermal nonequilibrium and finite-rate chemistry % % % -% Author: C. Garbacz % +% Author: C. Garbacz % % Institution: Strathclyde University % % Date: 2019.04.10 % % File Version 7.1.1 "Blackbird" % diff --git a/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg b/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg index 8a46ede2a28..7e6cc6cd8a0 100644 --- a/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg +++ b/TestCases/nonequilibrium/thermalbath/frozen/thermalbath_frozen.cfg @@ -3,7 +3,7 @@ % SU2 configuration file % % Case description: 2D 5x5 Sqaure Test Case % % % -% Author: C. Garbacz % +% Author: C. Garbacz % % Institution: Strathclyde University % % Date: 2019.04.10 % % File Version 7.1.1 "Blackbird" % diff --git a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg index c6b69b57b33..d24de29bff2 100644 --- a/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg +++ b/TestCases/optimization_euler/steady_inverse_design/inv_NACA0012.cfg @@ -5,7 +5,7 @@ % Author: Thomas D. Economon % % Institution: Stanford University % % Date: 2014.06.11 % -% File Version 7.1.1 "Blackbird % +% File Version 3.2.7 "eagle" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/rans/naca0012/turb_NACA0012_sa.cfg b/TestCases/rans/naca0012/turb_NACA0012_sa.cfg index 46d95de0243..e7d981efd45 100644 --- a/TestCases/rans/naca0012/turb_NACA0012_sa.cfg +++ b/TestCases/rans/naca0012/turb_NACA0012_sa.cfg @@ -3,7 +3,7 @@ % SU2 configuration file % % Case description: 2D NACA 0012 Airfoil Validation Case (compressible) % % http://turbmodels.larc.nasa.gov/naca0012_val_sa.html % -% Author: Francisco Palacios % +% Author: Francisco Palacios % % Institution: Stanford University % % Date: Feb 18th, 2013 % % File Version 7.1.1 "Blackbird % diff --git a/TestCases/rans/naca0012/turb_NACA0012_sa_binary.cfg b/TestCases/rans/naca0012/turb_NACA0012_sa_binary.cfg deleted file mode 100644 index b579467180c..00000000000 --- a/TestCases/rans/naca0012/turb_NACA0012_sa_binary.cfg +++ /dev/null @@ -1,252 +0,0 @@ -%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% -% % -% SU2 configuration file % -% Case description: 2D NACA 0012 Airfoil Validation Case (compressible) % -% http://turbmodels.larc.nasa.gov/naca0012_val_sa.html % -% Author: Francisco Palacios % -% Institution: Stanford University % -% Date: Feb 18th, 2013 % -% File Version 7.1.1 "Blackbird % -% % -%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% - -% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------% -% -% Physical governing equations (EULER, NAVIER_STOKES, -% WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY, -% POISSON_EQUATION) -SOLVER= RANS -% -% Specify turbulent model (NONE, SA, SA_NEG, SST) -KIND_TURB_MODEL= SA -% -% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT) -MATH_PROBLEM= DIRECT -% -% Restart solution (NO, YES) -RESTART_SOL= YES -% -% Discard the data storaged in the solution and geometry files -% e.g. AOA, dCL/dAoA, dCD/dCL, iter, etc. -% Note that AoA in the solution and geometry files is critical -% to aero design using AoA as a variable. (NO, YES) -DISCARD_INFILES= YES -% -% Read binary restart files (YES, NO) -READ_BINARY_RESTART= YES -% - -% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------% -% -% Mach number (non-dimensional, based on the free-stream values) -MACH_NUMBER= 0.15 -% -% Angle of attack (degrees, only for compressible flows) -AOA= 10.0 -% -% Free-stream temperature (288.15 K by default) -FREESTREAM_TEMPERATURE= 300.0 -% -% Reynolds number (non-dimensional, based on the free-stream values) -REYNOLDS_NUMBER= 6.0E6 -% -% Reynolds length (1 m by default) -REYNOLDS_LENGTH= 1.0 - -% ---------------------- REFERENCE VALUE DEFINITION ---------------------------% -% -% Reference origin for moment computation -REF_ORIGIN_MOMENT_X = 0.25 -REF_ORIGIN_MOMENT_Y = 0.00 -REF_ORIGIN_MOMENT_Z = 0.00 -% -% Reference length for pitching, rolling, and yawing non-dimensional moment -REF_LENGTH= 1.0 -% -% Reference area for force coefficients (0 implies automatic calculation) -REF_AREA= 1.0 -% -% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE, -% FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE) -REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE - -% -------------------- BOUNDARY CONDITION DEFINITION --------------------------% -% -% Navier-Stokes wall boundary marker(s) (NONE = no marker) -MARKER_HEATFLUX= ( airfoil, 0.0 ) -% -% Farfield boundary marker(s) (NONE = no marker) -MARKER_FAR= ( farfield ) -% -% Marker(s) of the surface to be plotted or designed -MARKER_PLOTTING= ( airfoil ) -% -% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated -MARKER_MONITORING= ( airfoil ) - -% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------% -% -% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES) -NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES -% -% Courant-Friedrichs-Lewy condition of the finest grid -CFL_NUMBER= 10.0 -% -% Max Delta time -MAX_DELTA_TIME= 1E10 -% -% Adaptive CFL number (NO, YES) -CFL_ADAPT= NO -% -% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, -% CFL max value ) -CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 ) -% -% Number of total iterations -ITER= 99999 - -% ----------------------- SLOPE LIMITER DEFINITION ----------------------------% -% -% Coefficient for the limiter -VENKAT_LIMITER_COEFF= 0.03 -% -% Freeze the value of the limiter after a number of iterations -LIMITER_ITER= 99999 - -% ------------------------ LINEAR SOLVER DEFINITION ---------------------------% -% -% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER) -LINEAR_SOLVER= FGMRES -% -% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI) -LINEAR_SOLVER_PREC= LU_SGS -% -% Minimum error of the linear solver for implicit formulations -LINEAR_SOLVER_ERROR= 1E-10 -% -% Max number of iterations of the linear solver for the implicit formulation -LINEAR_SOLVER_ITER= 5 - -% -------------------------- MULTIGRID PARAMETERS -----------------------------% -% -% Multi-Grid Levels (0 = no multi-grid) -MGLEVEL= 0 -% -% Multigrid pre-smoothing level -MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1, 1 ) -% -% Multigrid post-smoothing level -MG_POST_SMOOTH= ( 0, 0, 0, 0, 0, 0 ) -% -% Jacobi implicit smoothing of the correction -MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0, 0, 0 ) -% -% Damping factor for the residual restriction -MG_DAMP_RESTRICTION= 0.75 -% -% Damping factor for the correction prolongation -MG_DAMP_PROLONGATION= 0.75 - -% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------% -% -% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC, -% TURKEL_PREC, MSW) -CONV_NUM_METHOD_FLOW= ROE -% -% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER) -MUSCL_FLOW= YES -% -% Slope limiter (VENKATAKRISHNAN, MINMOD) -SLOPE_LIMITER_FLOW= VENKATAKRISHNAN -% -% 2nd and 4th order artificial dissipation coefficients -JST_SENSOR_COEFF= ( 0.5, 0.02 ) -% -% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT) -TIME_DISCRE_FLOW= EULER_IMPLICIT - -% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------% -% -% Convective numerical method (SCALAR_UPWIND) -CONV_NUM_METHOD_TURB= SCALAR_UPWIND -% -% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations. -% Required for 2nd order upwind schemes (NO, YES) -MUSCL_TURB= YES -% -% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG, -% BARTH_JESPERSEN, VAN_ALBADA_EDGE) -SLOPE_LIMITER_TURB= NONE -% -% Time discretization (EULER_IMPLICIT) -TIME_DISCRE_TURB= EULER_IMPLICIT -% -% Reduction factor of the CFL coefficient in the turbulence problem -CFL_REDUCTION_TURB= 1.0 - -% --------------------------- CONVERGENCE PARAMETERS --------------------------% -% -% Min value of the residual (log10 of the residual) -CONV_RESIDUAL_MINVAL= -12 -% -% Start convergence criteria at iteration number -CONV_STARTITER= 10 -% -% Number of elements to apply the criteria -CONV_CAUCHY_ELEMS= 100 -% -% Epsilon to control the series convergence -CONV_CAUCHY_EPS= 1E-6 -% - -% ------------------------- INPUT/OUTPUT INFORMATION --------------------------% -% -% Mesh input file -MESH_FILENAME= n0012_225-65.su2 -% -% Mesh input file format (SU2, CGNS, NETCDF_ASCII) -MESH_FORMAT= SU2 -% -% Mesh output file -MESH_OUT_FILENAME= mesh_out.su2 -% -% Restart flow input file -SOLUTION_FILENAME= solution_flow_sa_bin.dat -% -% Restart adjoint input file -SOLUTION_ADJ_FILENAME= solution_adj.dat -% -% Output file format (PARAVIEW, TECPLOT, STL) -TABULAR_FORMAT= CSV -% -% Output file convergence history (w/o extension) -CONV_FILENAME= history -% -% Output file restart flow -RESTART_FILENAME= restart_flow.dat -% -% Output file restart adjoint -RESTART_ADJ_FILENAME= restart_adj.dat -% -% Output file flow (w/o extension) variables -VOLUME_FILENAME= flow -% -% Output file adjoint (w/o extension) variables -VOLUME_ADJ_FILENAME= adjoint -% -% Output objective function gradient (using continuous adjoint) -GRAD_OBJFUNC_FILENAME= of_grad.dat -% -% Output file surface flow coefficient (w/o extension) -SURFACE_FILENAME= surface_flow -% -% Output file surface adjoint coefficient (w/o extension) -SURFACE_ADJ_FILENAME= surface_adjoint -% -% Writing solution file frequency -OUTPUT_WRT_FREQ= 10000 -% -% -% Screen output fields -SCREEN_OUTPUT= (INNER_ITER, RMS_DENSITY, RMS_NU_TILDE, LIFT, DRAG) - diff --git a/TestCases/rans/naca0012/turb_NACA0012_sa_neg.cfg b/TestCases/rans/naca0012/turb_NACA0012_sa_neg.cfg deleted file mode 100644 index 2a84ec66f3a..00000000000 --- a/TestCases/rans/naca0012/turb_NACA0012_sa_neg.cfg +++ /dev/null @@ -1,239 +0,0 @@ -%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% -% % -% SU2 configuration file % -% Case description: 2D NACA 0012 Airfoil Validation Case (compressible) % -% http://turbmodels.larc.nasa.gov/naca0012_val_sa.html % -% Author: Francisco Palacios % -% Institution: Stanford University % -% Date: Feb 18th, 2013 % -% File Version 7.1.1 "Blackbird % -% % -%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% - -% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------% -% -% Physical governing equations (EULER, NAVIER_STOKES, -% WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY, -% POISSON_EQUATION) -SOLVER= RANS -% -% Specify turbulent model (NONE, SA, SA_NEG, SST) -KIND_TURB_MODEL= SA_NEG -% -% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT) -MATH_PROBLEM= DIRECT -% -% Restart solution (NO, YES) -RESTART_SOL= YES -% - -% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------% -% -% Mach number (non-dimensional, based on the free-stream values) -MACH_NUMBER= 0.15 -% -% Angle of attack (degrees, only for compressible flows) -AOA= 10.0 -% -% Free-stream temperature (288.15 K by default) -FREESTREAM_TEMPERATURE= 300.0 -% -% Reynolds number (non-dimensional, based on the free-stream values) -REYNOLDS_NUMBER= 6.0E6 -% -% Reynolds length (1 m by default) -REYNOLDS_LENGTH= 1.0 - -% ---------------------- REFERENCE VALUE DEFINITION ---------------------------% -% -% Reference origin for moment computation -REF_ORIGIN_MOMENT_X = 0.25 -REF_ORIGIN_MOMENT_Y = 0.00 -REF_ORIGIN_MOMENT_Z = 0.00 -% -% Reference length for pitching, rolling, and yawing non-dimensional moment -REF_LENGTH= 1.0 -% -% Reference area for force coefficients (0 implies automatic calculation) -REF_AREA= 1.0 -% -% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE, -% FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE) -REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE - -% -------------------- BOUNDARY CONDITION DEFINITION --------------------------% -% -% Navier-Stokes wall boundary marker(s) (NONE = no marker) -MARKER_HEATFLUX= ( airfoil, 0.0 ) -% -% Farfield boundary marker(s) (NONE = no marker) -MARKER_FAR= ( farfield ) -% -% Marker(s) of the surface to be plotted or designed -MARKER_PLOTTING= ( airfoil ) -% -% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated -MARKER_MONITORING= ( airfoil ) - -% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------% -% -% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES) -NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES -% -% Courant-Friedrichs-Lewy condition of the finest grid -CFL_NUMBER= 10.0 -% -% Max Delta time -MAX_DELTA_TIME= 1E10 -% -% Adaptive CFL number (NO, YES) -CFL_ADAPT= NO -% -% Parameters of the adaptive CFL number (factor down, factor up, CFL min value, -% CFL max value ) -CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 ) -% -% Number of total iterations -EXT_ITER= 25 - -% ----------------------- SLOPE LIMITER DEFINITION ----------------------------% -% -% Coefficient for the limiter -VENKAT_LIMITER_COEFF= 0.03 -% -% Freeze the value of the limiter after a number of iterations -LIMITER_ITER= 99999 - -% ------------------------ LINEAR SOLVER DEFINITION ---------------------------% -% -% Linear solver or smoother for implicit formulations (BCGSTAB, FGMRES, SMOOTHER) -LINEAR_SOLVER= FGMRES -% -% Preconditioner of the Krylov linear solver (ILU, LU_SGS, LINELET, JACOBI) -LINEAR_SOLVER_PREC= LU_SGS -% -% Minimum error of the linear solver for implicit formulations -LINEAR_SOLVER_ERROR= 1E-10 -% -% Max number of iterations of the linear solver for the implicit formulation -LINEAR_SOLVER_ITER= 5 - -% -------------------------- MULTIGRID PARAMETERS -----------------------------% -% -% Multi-Grid Levels (0 = no multi-grid) -MGLEVEL= 0 -% -% Multigrid pre-smoothing level -MG_PRE_SMOOTH= ( 1, 1, 1, 1, 1, 1 ) -% -% Multigrid post-smoothing level -MG_POST_SMOOTH= ( 0, 0, 0, 0, 0, 0 ) -% -% Jacobi implicit smoothing of the correction -MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0, 0, 0 ) -% -% Damping factor for the residual restriction -MG_DAMP_RESTRICTION= 0.75 -% -% Damping factor for the correction prolongation -MG_DAMP_PROLONGATION= 0.75 - -% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------% -% -% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC, -% TURKEL_PREC, MSW) -CONV_NUM_METHOD_FLOW= ROE -% -% Spatial numerical order integration (1ST_ORDER, 2ND_ORDER, 2ND_ORDER_LIMITER) -MUSCL_FLOW= YES -% -% Slope limiter (VENKATAKRISHNAN, MINMOD) -SLOPE_LIMITER_FLOW= VENKATAKRISHNAN -% -% 2nd and 4th order artificial dissipation coefficients -JST_SENSOR_COEFF= ( 0.5, 0.02 ) -% -% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT) -TIME_DISCRE_FLOW= EULER_IMPLICIT - -% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------% -% -% Convective numerical method (SCALAR_UPWIND) -CONV_NUM_METHOD_TURB= SCALAR_UPWIND -% -% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations. -% Required for 2nd order upwind schemes (NO, YES) -MUSCL_TURB= YES -% -% Slope limiter (NONE, VENKATAKRISHNAN, VENKATAKRISHNAN_WANG, -% BARTH_JESPERSEN, VAN_ALBADA_EDGE) -SLOPE_LIMITER_TURB= NONE -% -% Time discretization (EULER_IMPLICIT) -TIME_DISCRE_TURB= EULER_IMPLICIT -% -% Reduction factor of the CFL coefficient in the turbulence problem -CFL_REDUCTION_TURB= 1.0 - -% --------------------------- CONVERGENCE PARAMETERS --------------------------% -% -% Min value of the residual (log10 of the residual) -CONV_RESIDUAL_MINVAL= -12 -% -% Start convergence criteria at iteration number -CONV_STARTITER= 10 -% -% Number of elements to apply the criteria -CONV_CAUCHY_ELEMS= 100 -% -% Epsilon to control the series convergence -CONV_CAUCHY_EPS= 1E-6 -% - -% ------------------------- INPUT/OUTPUT INFORMATION --------------------------% -% -% Mesh input file -MESH_FILENAME= n0012_897-257.su2 -% -% Mesh input file format (SU2, CGNS, NETCDF_ASCII) -MESH_FORMAT= SU2 -% -% Mesh output file -MESH_OUT_FILENAME= mesh_out.su2 -% -% Restart flow input file -SOLUTION_FILENAME= solution_flow_sa.dat -% -% Restart adjoint input file -SOLUTION_ADJ_FILENAME= solution_adj.dat -% -% Output file format (PARAVIEW, TECPLOT, STL) -TABULAR_FORMAT= CSV -% -% Output file convergence history (w/o extension) -CONV_FILENAME= history -% -% Output file restart flow -RESTART_FILENAME= restart_flow.dat -% -% Output file restart adjoint -RESTART_ADJ_FILENAME= restart_adj.dat -% -% Output file flow (w/o extension) variables -VOLUME_FILENAME= flow -% -% Output file adjoint (w/o extension) variables -VOLUME_ADJ_FILENAME= adjoint -% -% Output objective function gradient (using continuous adjoint) -GRAD_OBJFUNC_FILENAME= of_grad.dat -% -% Output file surface flow coefficient (w/o extension) -SURFACE_FILENAME= surface_flow -% -% Output file surface adjoint coefficient (w/o extension) -SURFACE_ADJ_FILENAME= surface_adjoint -% -% Writing solution file frequency -OUTPUT_WRT_FREQ= 10000 -% diff --git a/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg b/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg index f13f54b3792..219938c9369 100644 --- a/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg +++ b/TestCases/sliding_interface/channel_2D/channel_2D_NN.cfg @@ -4,7 +4,7 @@ % Case description: 2D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg b/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg index 3b6183fd7c3..afcb8d38ac0 100644 --- a/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg +++ b/TestCases/sliding_interface/channel_2D/channel_2D_WA.cfg @@ -4,7 +4,7 @@ % Case description: 2D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg b/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg index ded31611626..3a01e5e3e0c 100644 --- a/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg +++ b/TestCases/sliding_interface/channel_3D/channel_3D_NN.cfg @@ -4,7 +4,7 @@ % Case description: 3D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg b/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg index f8101410074..4c6bfc5ccfb 100644 --- a/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg +++ b/TestCases/sliding_interface/channel_3D/channel_3D_WA.cfg @@ -4,7 +4,7 @@ % Case description: 3D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/channel_3D/zone_1.cfg b/TestCases/sliding_interface/channel_3D/zone_1.cfg index b8f197a033b..54dad5dee40 100644 --- a/TestCases/sliding_interface/channel_3D/zone_1.cfg +++ b/TestCases/sliding_interface/channel_3D/zone_1.cfg @@ -4,7 +4,7 @@ % Case description: 3D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/channel_3D/zone_2.cfg b/TestCases/sliding_interface/channel_3D/zone_2.cfg index 937a5b0a5f5..ed55ec48e97 100644 --- a/TestCases/sliding_interface/channel_3D/zone_2.cfg +++ b/TestCases/sliding_interface/channel_3D/zone_2.cfg @@ -4,7 +4,7 @@ % Case description: 3D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/channel_3D/zone_3.cfg b/TestCases/sliding_interface/channel_3D/zone_3.cfg index 0e42d310305..48421ea9019 100644 --- a/TestCases/sliding_interface/channel_3D/zone_3.cfg +++ b/TestCases/sliding_interface/channel_3D/zone_3.cfg @@ -4,7 +4,7 @@ % Case description: 3D, inviscid flow inside a channel with a partially % % moving grid, nearest neighbour approach holds at interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/incompressible_unsteady/config.cfg b/TestCases/sliding_interface/incompressible_unsteady/config.cfg index 2bbbbb98c8a..81a7c8bbf02 100644 --- a/TestCases/sliding_interface/incompressible_unsteady/config.cfg +++ b/TestCases/sliding_interface/incompressible_unsteady/config.cfg @@ -5,7 +5,7 @@ % Author: Ruben Sanchez % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: January 28th, 2018 % -% File Version 7.1.1 "Blackbird" % +% File Version 6.1.0 "Falcon" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg b/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg index a196ffdea01..4082db97ddf 100644 --- a/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg +++ b/TestCases/sliding_interface/incompressible_unsteady/configCircle.cfg @@ -5,7 +5,7 @@ % Author: Ruben Sanchez % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: January 28th, 2018 % -% File Version 7.1.1 "Blackbird" % +% File Version 6.1.0 "Falcon" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg b/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg index be56fac04c1..c104e40ec79 100644 --- a/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg +++ b/TestCases/sliding_interface/incompressible_unsteady/configOut.cfg @@ -5,7 +5,7 @@ % Author: Ruben Sanchez % % Institution: Chair for Scientific Computing, TU Kaiserslautern % % Date: January 28th, 2018 % -% File Version 7.1.1 "Blackbird" % +% File Version 6.1.0 "Falcon" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/pipe/pipe_NN.cfg b/TestCases/sliding_interface/pipe/pipe_NN.cfg index d4c4c4d14ac..6d6629d1558 100644 --- a/TestCases/sliding_interface/pipe/pipe_NN.cfg +++ b/TestCases/sliding_interface/pipe/pipe_NN.cfg @@ -4,7 +4,7 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/pipe/pipe_WA.cfg b/TestCases/sliding_interface/pipe/pipe_WA.cfg index 8ad225ba535..8d99090aa30 100644 --- a/TestCases/sliding_interface/pipe/pipe_WA.cfg +++ b/TestCases/sliding_interface/pipe/pipe_WA.cfg @@ -4,7 +4,7 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/pipe/zone_1.cfg b/TestCases/sliding_interface/pipe/zone_1.cfg index f238407ffaf..c82e86511b5 100644 --- a/TestCases/sliding_interface/pipe/zone_1.cfg +++ b/TestCases/sliding_interface/pipe/zone_1.cfg @@ -4,7 +4,7 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/pipe/zone_2.cfg b/TestCases/sliding_interface/pipe/zone_2.cfg index 7e30feded3a..5d18b84ccad 100644 --- a/TestCases/sliding_interface/pipe/zone_2.cfg +++ b/TestCases/sliding_interface/pipe/zone_2.cfg @@ -4,7 +4,7 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/pipe/zone_3.cfg b/TestCases/sliding_interface/pipe/zone_3.cfg index e70627cbf24..3ac397f5bc9 100644 --- a/TestCases/sliding_interface/pipe/zone_3.cfg +++ b/TestCases/sliding_interface/pipe/zone_3.cfg @@ -4,7 +4,7 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/pipe/zone_4.cfg b/TestCases/sliding_interface/pipe/zone_4.cfg index 0b7d28345f6..ad88c75938b 100644 --- a/TestCases/sliding_interface/pipe/zone_4.cfg +++ b/TestCases/sliding_interface/pipe/zone_4.cfg @@ -4,7 +4,7 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/pipe/zone_5.cfg b/TestCases/sliding_interface/pipe/zone_5.cfg index e6db5eecea9..0274bc59836 100644 --- a/TestCases/sliding_interface/pipe/zone_5.cfg +++ b/TestCases/sliding_interface/pipe/zone_5.cfg @@ -4,7 +4,7 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg index c44185acc4e..cba6f7a4c87 100644 --- a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg +++ b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_NN.cfg @@ -3,7 +3,7 @@ % SU2 configuration file % % Case description: 2D, four cylynders rotating inside a supersonic flow % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg index 551dc1745e7..c61d4ccfbaf 100644 --- a/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg +++ b/TestCases/sliding_interface/rotating_cylinders/rot_cylinders_WA.cfg @@ -3,7 +3,7 @@ % SU2 configuration file % % Case description: 2D, four cylynders rotating inside a supersonic flow % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/single_stage/single_stage_NN.cfg b/TestCases/sliding_interface/single_stage/single_stage_NN.cfg index 6ada93b0aae..d84aa9b0576 100644 --- a/TestCases/sliding_interface/single_stage/single_stage_NN.cfg +++ b/TestCases/sliding_interface/single_stage/single_stage_NN.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 7.1.1 "Blackbird" % +% File Version 4.3.0 "cardinal" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/single_stage/single_stage_WA.cfg b/TestCases/sliding_interface/single_stage/single_stage_WA.cfg index c5a70f92f26..b04adedd0d9 100644 --- a/TestCases/sliding_interface/single_stage/single_stage_WA.cfg +++ b/TestCases/sliding_interface/single_stage/single_stage_WA.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 7.1.1 "Blackbird" % +% File Version 4.3.0 "cardinal" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/sliding_interface/single_stage/zone_1.cfg b/TestCases/sliding_interface/single_stage/zone_1.cfg index cfbcf1afde0..46c87be7073 100644 --- a/TestCases/sliding_interface/single_stage/zone_1.cfg +++ b/TestCases/sliding_interface/single_stage/zone_1.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 7.1.1 "Blackbird" % +% File Version 4.3.0 "cardinal" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/single_stage/zone_2.cfg b/TestCases/sliding_interface/single_stage/zone_2.cfg index c35971a3b23..27de8c25b1f 100644 --- a/TestCases/sliding_interface/single_stage/zone_2.cfg +++ b/TestCases/sliding_interface/single_stage/zone_2.cfg @@ -4,9 +4,9 @@ % Case description: 3D, inviscid flow inside a pipe with rotating sections % % nearest neighbour approach holds at sliding interface % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % -% File Version 7.1.1 "Blackbird" % +% File Version 4.3.0 "cardinal" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg index 6ebd99563ec..3958dae228e 100644 --- a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg +++ b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_NN.cfg @@ -4,7 +4,7 @@ % Case description: 2D inviscid, this test case reproduces vortex shedding % % after a cylindrical body in a supersonic upstream flow % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg index 4c53e46103d..5e7e7843ac9 100644 --- a/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg +++ b/TestCases/sliding_interface/supersonic_vortex_shedding/sup_vor_shed_WA.cfg @@ -4,7 +4,7 @@ % Case description: 2D inviscid, this test case reproduces vortex shedding % % after a cylindrical body in a supersonic upstream flow % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg index dd85801b80d..4dc523dc0cc 100644 --- a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg +++ b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_1.cfg @@ -4,7 +4,7 @@ % Case description: 2D inviscid, this test case reproduces vortex shedding % % after a cylindrical body in a supersonic upstream flow % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg index bcd85355708..fa40651b182 100644 --- a/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg +++ b/TestCases/sliding_interface/supersonic_vortex_shedding/zone_2.cfg @@ -4,7 +4,7 @@ % Case description: 2D inviscid, this test case reproduces vortex shedding % % after a cylindrical body in a supersonic upstream flow % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg b/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg index 34f7b0f7613..b31ade0996b 100644 --- a/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg +++ b/TestCases/sliding_interface/uniform_flow/uniform_NN.cfg @@ -4,7 +4,7 @@ % Case description: 2D, inviscid flow, this test case is used for debugging % % purposes, part of the grid is moving % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg b/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg index 492db3a2cf3..5c49e974323 100644 --- a/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg +++ b/TestCases/sliding_interface/uniform_flow/uniform_WA.cfg @@ -4,7 +4,7 @@ % Case description: 2D, inviscid flow, this test case is used for debugging % % purposes, part of the grid is moving % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/uniform_flow/zone_1.cfg b/TestCases/sliding_interface/uniform_flow/zone_1.cfg index 399bdc2f868..2b15853dbe0 100644 --- a/TestCases/sliding_interface/uniform_flow/zone_1.cfg +++ b/TestCases/sliding_interface/uniform_flow/zone_1.cfg @@ -4,7 +4,7 @@ % Case description: 2D, inviscid flow, this test case is used for debugging % % purposes, part of the grid is moving % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/sliding_interface/uniform_flow/zone_2.cfg b/TestCases/sliding_interface/uniform_flow/zone_2.cfg index b1c64f70a42..0f51630bb9d 100644 --- a/TestCases/sliding_interface/uniform_flow/zone_2.cfg +++ b/TestCases/sliding_interface/uniform_flow/zone_2.cfg @@ -4,7 +4,7 @@ % Case description: 2D, inviscid flow, this test case is used for debugging % % purposes, part of the grid is moving % % Author: G. Gori % -% Institution: Politecnico di Milano % +% Institution: Politecnico di Milano % % Date: Oct 5th, 2016 % % File Version 7.1.1 "Blackbird" % % % diff --git a/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg b/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg index 119320318e3..4066a0420dc 100755 --- a/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg +++ b/TestCases/turbomachinery/centrifugal_blade/centrifugal_blade.cfg @@ -2,10 +2,10 @@ % % % SU2 configuration file % % Case description: Centrifugal turbine rotor % -% Author:S. Vitale % +% Author:S. Vitale % % Institution: Delft University of Technology % % Date: Oct 26th, 2015 % -% File Version 7.1.1 "Blackbird" % +% File Version 4.0.1 "cardinal" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg b/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg index 7031b42b19d..69740ee71b8 100755 --- a/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg +++ b/TestCases/turbomachinery/centrifugal_stage/centrifugal_stage.cfg @@ -5,7 +5,7 @@ % Author: S. Vitale % % Institution: Delft University of Technology % % Date: Oct 28th, 2015 % -% File Version 7.1.1 "Blackbird" % +% File Version 4.0.1 "cardinal" % % % %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % diff --git a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator.cfg b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator.cfg index 42f76d6afd0..2413c86a268 100644 --- a/TestCases/turbomachinery/transonic_stator_2D/transonic_stator.cfg +++ b/TestCases/turbomachinery/transonic_stator_2D/transonic_stator.cfg @@ -1,7 +1,7 @@ %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% % % % SU2 configuration file % -% Case description: Transonic ORC nozzle % +% Case description: Transonic ORC nozzle % % Author: S. Vitale % % Institution: Delft University of Technology % % Date: 2017.03.01 %