AIAA-2004-5193 Subsonic Aerodynamic Fin Folding Moments for the Tactical Tomahawk Missile Configuration
22nd, AIAA applied aerodynamics conference ; 2004 ; Providence, RI
AIAA applied aerodynamics conference ; 823-831
01.01.2004
9 pages
Aufsatz (Konferenz)
Englisch
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