Wind tunnel tests and computational analysis of the CAN1A projectile at Mach 8.2
34th Aerospace Sciences Meeting and Exhibit ; 1996 ; Reno , NV , U.S.A.
01.01.1996
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
AIAA 2000-0105 Wind Tunnel Tests of a Grid Finned Projectile Configuration
British Library Conference Proceedings | 2001
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