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adiabatic wall AIAA analytic approximations APPENDIX axisymmetric body Blunt Bodies body shapes boundary conditions boundary layer bow shock calculated cell walls cold wall comparisons component of velocity computational space continuum theory cosh derivatives with respect difference approximations drag coefficient ENTHALPY DERIVATIVE experimental data flux forebody free-stream governing equations h 3r heat transfer i,NJ inviscid iterations Jupiter probe Knudsen number Laminar Mach number mean free path mesh points metric coefficients nAnenr NASA Navier-Stokes equations negative static enthalpies no-slip condition nondimensionalized number and Reynolds number of mesh Numerical Solutions obtained orthogonal coordinate system outflow boundary planetary probe pn+1 presented in figure pressure coefficient Pressure coefficient distribution Reynolds number range shock layer shock standoff distance sinh stability limit stagnation region stretching parameter supersonic flow Sutherland's law symmetry line technique temperature slip tions transformed coordinate system values Viking aeroshell viscous wall temperature x,y plane Ymax