AIAA-2003-3805 Deflectable Nose and Canard Controls for a Fin-Stabilized Projectile at Supersonic and Hypersonic Speeds
Conference; 21st, Applied aerodynamics ; 2003 ; Orlando, FL
2003-01-01
15 pages
Aufsatz (Konferenz)
Englisch
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Hinge Moment Coefficient Prediction for Nose-Mounted Canard Controls at Supersonic Speeds
Online Contents | 1998
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