High-Reynolds-number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions
By: Julio Chu and Pierce L. Lawing.
Contributors: Lawing, Pierce L.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4189.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1990
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Airplanes -- Wings.; Transonic wind tunnels.
Other titles: High Reynolds number test of a 5-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wing tunnel distributions.; High-Reynolds-number test of a five-percent-thick low-aspect-ratio semispan wing in the Langley 0.3-meter transonic cryogenic tunnel, wind tunnel distributions.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 93-1213-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1993] 3 microfiches.