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

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