Numerical study of induced nonlinear rolling moment of finned missile at high angles of attack
Hang kong xue bao ; 35 , 1 ; 97-104
2014
Aufsatz (Zeitschrift)
Chinesisch
Missile loads at high angles of attack
AIAA | 1991
|Missile Loads at High Angles of Attack
AIAA | 1991
|Numerical Prediction of Pitch Damping Derivatives for a Finned Projectile at Angles of Attack
British Library Conference Proceedings | 2012
|