Experimental Investigation of the Stability, Control, and Induced Rolling Moments of a Canard Missile Airframe at a Mach Number of 1.7
1952-09-23
Sonstige
Keine Angabe
Englisch
Aerodynamics of a Rolling Airframe Missile
NTIS | 1981
|Modeling Jamming Effects on Rolling Airframe Missile
NTIS | 2001
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