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Add nemo inviscid wedge tutorial #37

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09b1c21
adding nemo wedge tutorial
jtneedels Jan 23, 2023
5cfcfec
remove ds store
jtneedels Jan 23, 2023
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52,110 changes: 52,110 additions & 0 deletions nemo/Inviscid_Hypersonic_Wedge/invwedge.su2
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76 changes: 76 additions & 0 deletions nemo/Inviscid_Hypersonic_Wedge/invwedge_ausm.cfg
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
% %
% SU2 configuration file %
% Case description: Mach 5 inviscid flow over a 10deg wedge-AUSM %
% Author: C. Garbacz %
% Institution: Strathclyde University %
% Date: 2020.11.01 %
% File Version 7.5.0 "Blackbird" %
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% File Version 7.5.0 "Blackbird" %
% File Version 7.5.1 "Blackbird" %

% %
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%

% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
%
SOLVER= NEMO_EULER
GAS_MODEL= AIR-5
GAS_COMPOSITION= (0.77, 0.23, 0.0, 0.0, 0.0)
MATH_PROBLEM= DIRECT
RESTART_SOL= NO

% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
%
MACH_NUMBER= 5
AOA= 0.0
SIDESLIP_ANGLE= 0.0
FREESTREAM_PRESSURE= 101325.0
FREESTREAM_TEMPERATURE= 288.15
FREESTREAM_TEMPERATURE_VE= 288.15

% ---- NONEQUILIBRIUM GAS, IDEAL GAS, POLYTROPIC, VAN DER WAALS AND PENG ROBINSON CONSTANTS -------%
%
FLUID_MODEL= SU2_NONEQ

% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
%
MARKER_EULER= ( Euler, Wall )
MARKER_OUTLET= ( Exit, 10 )
MARKER_FAR = ( Farfield, Inlet )
MARKER_PLOTTING= (NONE )
MARKER_MONITORING= ( Wall )

% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
%
NUM_METHOD_GRAD= WEIGHTED_LEAST_SQUARES
CFL_NUMBER= 3
ITER= 99999
LINEAR_SOLVER= BCGSTAB
LINEAR_SOLVER_ERROR= 1E-6
LINEAR_SOLVER_ITER= 5

% -----------------------------------------------------------------------%
%
CONV_NUM_METHOD_FLOW= AUSM
MUSCL_FLOW= YES
SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
VENKAT_LIMITER_COEFF= 0.05
TIME_DISCRE_FLOW= EULER_IMPLICIT

% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
CONV_RESIDUAL_MINVAL= -10
CONV_STARTITER= 10
CONV_CAUCHY_ELEMS= 100
CONV_CAUCHY_EPS= 1E-10

% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
%
MESH_FILENAME= invwedge.su2
MESH_FORMAT= SU2
SOLUTION_FILENAME= restart_flow.dat
TABULAR_FORMAT= TECPLOT
CONV_FILENAME= convergence
RESTART_FILENAME= restart_flow.dat
VOLUME_FILENAME= soln_volume
SURFACE_FILENAME= soln_surface
OUTPUT_WRT_FREQ= 100
OUTPUT_FILES= (RESTART_ASCII, PARAVIEW_ASCII)