Supersonic hows past a blunt body in air and in water are numerically inves
tigated by using a high-resolution Euler/Navier-Stokes solver. The numerica
l method used is a fourth-order Runge-Kutta method for time integration wit
h a fifth-order weighted essentially nonoscillatory scheme for discretizing
the convective terms and central differencing for the viscous terms. The i
nviscid- and viscous-flow results are compared. It was found that the invis
cid-flow model is able to predict reasonably accurate flowfields such as th
e bow shock and sonic-line locations. Moreover, for the case of medium wate
r the bow-shock location is farther upstream, and the sonic line is farther
downstream compared with the case of medium air.