Jet-stream interaction effects on rocket engine studied with simulated ballistic missile using liquid oxygen and JP-4 fuel mixture
Experimental investigation of base heating and rocket hinge moments for a simulated missile through a Mach number range of 0.8 to 2.0
1959-10-01
Report
No indication
English
Aerodynamic Hinge Moments on a Sealed-Plain Trailing-Edge Flap at High Mach Number
British Library Conference Proceedings | 1991
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