Characterization of cavity flow fields using pressure data obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel
By: M.B. Tracy and E.B. Plentovich.
Contributors: Plentovich, Elizabeth B.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Series: NASA technical memorandum -- 4436.; NASA technical memorandum -- 4436.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; National Technical Information Service, distributor]
Published: 1993
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamics, Transonic.; Cavities (Airplanes)
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 93-0938-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1993] 1 microfiche.