"minimum mach number": 0.35
},
"turbulence": {
"model": "sst"
},
},
"material": "air",
"air": {
"gamma": 1.4,
"gas constant": 287.0,
"Sutherlands const": 110.4,
"Prandtl No": 0.72,
"Turbulent Prandtl No": 0.9,
},
"IC_1": {
"temperature": zutil.to_kelvin(540.0),
"pressure": 101325.0,
"V": {
"vector": zutil.vector_from_angle(alpha, 0.0),
"Mach": 0.15
},
#'viscosity' : 0.0,
"Reynolds No": 6.0e6,
"Reference Length": 1.0,
"turbulence intensity": 5.2e-2,
"eddy viscosity ratio": 1.0,
"ambient turbulence intensity": 5.2e-2,
"ambient eddy viscosity ratio": 1.0,
},
"BC_1": {
#'ref' : 3,
# Use linear gradients
'linear gradients': False,
# Optional (default 'HLLC'):
# Scheme for inviscid flux: HLLC or Rusanov
'Inviscid Flux Scheme': 'HLLC',
},
'material': 'air',
'air': {
'gamma': 1.4,
'gas constant': 287.0,
'Sutherlands const': 110.4,
'Prandtl No': 0.72,
'Turbulent Prandtl No': 0.9,
},
'IC_1': {
'temperature': zutil.to_kelvin(540.0),
'pressure': 101325.0,
'V': {
'vector': zutil.vector_from_angle(alpha, 0.0),
'Mach': 0.85,
},
# 'viscosity' : 0.0,
'Reynolds No': 6.0e6,
'Reference Length': 1.0,
'turbulence intensity': 5.2e-2,
'eddy viscosity ratio': 1.0,
'ambient turbulence intensity': 5.2e-2,
'ambient eddy viscosity ratio': 1.0,
},
'BC_1': {
# 'ref' : 3,