Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail

An edition of Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail (1996)

Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail

By Matthew Robert Whiting

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Publish Date

1996

Publisher

National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: X-31, Canard configurations, Directional control, Wind tunnel tests, Drop tests, Tail assemblies