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

Bibliographic Details
Main Author:	Johnson, William G. (William Garland), 1944-
Corporate Author:	Langley Research Center
Other Authors:	Hill, Acquilla S.
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1985.
Series:	NASA technical memorandum ; 87600.
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.
Online Access:	https://purl.fdlp.gov/GPO/LPS85654

Description
Item Description:	Prepared at Langley Research Center. Microform.
Physical Description:	1 volume 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.