Optimal pitch thrust-vector angle and benefits for all flight regimes

An edition of Optimal pitch thrust-vector angle and benefits for all flight regimes (2000)

Optimal pitch thrust-vector angle and benefits for all flight regimes

By Glenn B. Gilyard

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Publish Date

2000

Publisher

National Aeronautics and Space Administration, Dryden Flight Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Airplanes, Angles (Geometry), Automatic flight control, Control surfaces, Drag (Aerodynamics), Flight testing, Handling characteristics, Lift (Aerodynamics), Motors, Pitch (Inclination), Thrust, Thrust vector control