"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,