Water tunnel flow visualization study of a 4.4% scale X-31 forebody
By: Brent R. Cobleigh and John Del Frate.
Contributors: Frate, John Del.; Dryden Flight Research Facility.
Series: NASA technical memorandum -- 104276.
Publisher: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility; National Technical Information Service, distributor
Published: 1994
Place of publication: Edwards, Calif; [Springfield, Va
Language: eng
Format: Microform
Subjects: Angle of attack.; Asymmetry.; Flow visualization.; Forebodies.; Strakes.; Vortices.; Water tunnel tests.; X-31 aircraft.
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.