A Study to Determine the Accuracy of Two Computer Programs in Predicting Hinge Moments for all Movable Tail Fins on Missile Bodies.
ARMY MISSILE COMMAND REDSTONE ARSENAL AL SYSTEMS SIMULATION AND DEVELOPMENT DIRECTORATE
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The preliminary design of a guided missile with movable control surfaces requires an in-depth study of the aerodynamic loading experienced by these surfaces. Author.
- Guided Missiles
- Fluid Mechanics