Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
By: Stacey J. Cotton and Lisa J. Bjarke.
Contributors: Bjarke, Lisa J.; Hugh L. Dryden Flight Research Center.
Series: NASA technical memorandum -- 104268.
Publisher: National Aeronautics and Space Administration, Dryden Flight Research Center; National Technical Information Service, distributor
Published: 1994
Place of publication: Edwards, Calif; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic characteristics.; Angle of attack.; Buffeting.; Flight tests.; Flow visualization.; Liquid-vapor interfaces.; Scale models.; Sideslip.; Stabilizers (Fluid dynamics); Tail assemblies.; Vortices.; Water tunnel tests.; X-29 aircraft.
Other titles: Flow visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0058-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.