Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel /

Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel /

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Bibliographic Details
Author / Creator:	Schuster, D. M. (David M.)
Imprint:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
Description:	1 v.
Language:	English
Series:	[NASA technical memorandum] ; NASA/TM-2001-210828 NASA technical memorandum ; 210828.
Subject:	Transonic wind tunnels. Viscous flow.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/6529805

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Other authors / contributors:	Langley Research Center.
Notes:	Available via Internet from the NASA web site. Address as of 10/7/02: http://techreports.larc.nasa.gov/ltrs/PDF/2001/tm/NASA-2001-tm210828.pdf ; current access is available via PURL.
GPO item no.:	0830-D (MF) 0830-D (online)
Govt.docs classification:	NAS 1.15:210828

Description
Physical Description:	1 v.
Format:	Available via Internet from the NASA web site. Address as of 10/7/02: http://techreports.larc.nasa.gov/ltrs/PDF/2001/tm/NASA-2001-tm210828.pdf ; current access is available via PURL.