The methodology I am using was

Type- 2D Axis-symmetric behaviour

Flow domain is divided into finite number of unstructured quadrilateral cells

2D double precision, implicit, density based solver of flux type Roe-FDS

2 equation SST k-w turbulence model and RANS energy equations are solved

Air of ideal gas density as fluid with 3 coefficient Sutherland’s viscosity

Pressure far-field, stationary wall and ensured no slip condition

Free stream conditions

Mach number 6

Pressure 1064 Pa

Temperature 234 K

Thermal condition for wall : constant wall temperature of 300k

Turbulence intensity of 5% and Viscosity ratio of 10

Green gauss node based gradient

First order upwind discretization scheme for first few iterations and followed by second order upwind for further till convergence

Higher Order Term Relaxation, Convergence Acceleration for Structured Meshes and Warped face gradient correction were enabled

All the residuals were set to 1e-06

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