Report describes observations of supersonic flow of air over cylindrical body capped by hemisphere at its head and flared to cone at its tail end. Study prompted by need for greater aircraft control at high angles of attack.
Flow Over A Simplified-Rocket-Shaped Body
NASA Tech Briefs ; 16 , 2
1992-02-01
Sonstige
Keine Angabe
Englisch
Rocket body turning-over device and rocket hoisting system
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