Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail
By: by Matthew Robert Whiting.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA TM -- 111357.; NASA technical memorandum -- 111357.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Canard configurations.; Directional control.; Drop tests.; Tail assemblies.; Wind tunnel tests.; X-31.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0466-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1996] 2 microfiches.