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
29 pages
Report
Keine Angabe
Englisch
Rocket Engines & Motors , Missile Technology , Aerodynamics , Ballistic missile , Jet mixing , Jp-4 jet fuel , Liquid oxygen (lox) , Rocket engine , Afterbody , Ballistics , Base , Flow , Fuel , Heating , Hinge , Interaction , Jet , Liquid , Missile , Mixing , Moment , Oxygen , Pressure , Simulation , Stream , Temperature , Tunnel , Wind
Aerodynamic Hinge Moments on a Sealed-Plain Trailing-Edge Flap at High Mach Number
British Library Conference Proceedings | 1991
|