Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel /

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Bibliographic Details
Author / Creator:	Johnson, William G. (William Garland), 1944-
Imprint:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1985.
Description:	1 volume.
Language:	English
Series:	NASA technical memorandum ; 87600 NASA technical memorandum ; 87600.
Subject:	Aerofoils -- Testing -- Statistics. Aerodynamics, Transonic. Reynolds number.
Format:	E-Resource Microform U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/6808511

Hidden Bibliographic Details
Other authors / contributors:	Hill, Acquilla S. Langley Research Center.
Notes:	Prepared at Langley Research Center. 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.
GPO item no.:	0830-D (MF) 0830-D (online)
Govt.docs classification:	NAS 1.15:87600

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