This paper discusses some aspects of three-dimensional supersonic and
hypersonic inviscid blunt body how computations, The mehtod used is ba
sed on the solution of the Euler equations employing an explicit, upwi
nd total variation diminishing formulation of the Roe Riemann solver w
ithin the cell-centered finite volume approach. A comparative study of
various total variation diminishing limiters and entropy fixes is car
ried out to identify the most appropriate combination. The effect of u
sing cell spacing in the total variation diminishing extrapolations is
highlighted. Furthermore, a Mach number dependence and grid sensitivi
ty study is carried out on various total variation diminishing limiter
s scaled with mesh spacing. Local time stepping and code parallelizati
on has been employed to accelerate convergence in terms of effective w
ail clock times.