Comparisons between computational results and other computational results or experimental measurements of supersonic flows around tactical missiles are given. The presented results concern: aerodynamics of air-breathing missiles; vortex flows around conventional missiles, and flows with lateral streams (a problem encountered with devices applying lateral thrust near the center of gravity). The codes used at AEROSPATIALE fall in two categories: linearized, supersonic potential codes; Euler codes (steady and unsteady).
Calcul d'Ecoulements Supersoniques Autour de Missiles Tactiques (Calculation of Supersonic Flow around Tactical Missiles)
1986
32 pages
Report
No indication
English
MISSILES - Les missiles tactiques font le pari de la furtivité
Online Contents | 1998