Particle-in-cell method was used to obtain numerically full, time-dependent development of plane or cylindrical wake behind flat base of projectile moving with supersonic speed through air; particular attention is paid to case of Mach 1.89, arising from passage of very strong shock over projectile at rest; many features are shown of transient build-up to statistically steady state, as well as of late-time flow behavior.
Numerical calculation of supersonic wake flow
AIAA J
AIAA Journal ; 3 , n 11
1965
15 pages
Article (Journal)
English
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Numerical calculation of supersonic wake flow.
AIAA | 1965
|Supersonic wake flow visualization
AIAA | 1969
|Supersonic wake flow visualization
AIAA | 1969
|