High Reynolds number tests of the NASA SC(2)-0012 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
By: Raymond E. Mineck and Pierce L. Lawing.
Contributors: Lawing, Pierce L.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Series: NASA technical memorandum -- 89102.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1987
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Transonic wind tunnels.; Reynolds number.; Aerofoils -- Testing.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1987. 1 microfiche.