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
01.02.1992
Sonstige
Keine Angabe
Englisch
On Simplified Mechanical Models for Rocket-Body Divergence and Flutter
British Library Conference Proceedings | 2003
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