Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
By: William G. Johnson, Jr., and Acquilla S. Hill.
Contributors: Hill, Acquilla S.; Langley Research Center.
Series: NASA technical memorandum -- 87600.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1985
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerofoils -- Testing -- Statistics.; Aerodynamics, Transonic.; Reynolds number.; Airfoil profiles.; Boeing aircraft.; Cryogenic wind tunnels.; High Reynolds number.; Pressure distribution.; Supercritical airfoils.; Two dimensional bodies.; Wind tunnel models.; Wind tunnel tests.
Genres: Statistics.
Notes: Prepared at Langley Research Center.

Also available via Internet from the NTRS web site. Address as of 9/04/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860006729%5F1986006729.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 3 microfiches.