Numerical Aerodynamic Investigations on Missile Yawing Control Using Nose-Mounted Flow Effectors
Journal of Spacecraft and Rockets ; 45 , 2 ; 282-289
01.03.2008
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Numerical Aerodynamic Investigations on Missile Yawing Control Using Nose-Mounted Flow Effectors
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