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