Shape effects on hypersonic slender body wake geometry and transition distance.
WALDBUSSER, E. /GENERAL ELECTRIC CO., MISSILE AND SPACE DIV., RE-ENTRY SYSTEMS DEPT., PHILADELPHIA,
JOURNAL OF SPACECRAFT AND ROCKETS ; 4 , 5 ; 657-662
1967
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Hypersonic Slender Body Aerodynamics
TIBKAT | 2025
|Hypersonic slender body aerodynamics
TIBKAT | 2025
|AIAA | 1963
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