Abstract:
Some numerical results obtained for the case of spatial supersonic flow
around elements of a complex-shaped flying vehicle are presented. The
computations are performed on the basis of Euler equations. Analytical
relations used to construct the complicated geometry of vehicle
configurations are given.
For the Mach number $M_\infty = 4.03$ and the angle of attack
$\alpha = 10.1^\circ $, we analyze the numerical solutions to the problem of
spatial flow around an isolated ogival-cylindrical body, an isolated
delta wing with a diamond profile, and a body-wing combination.
Our numerical results are compared with data of physical experiments.