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

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Bibliographic Details
Main Author: Schuster, D. M. (David M.)
Corporate Author: Langley Research Center
Format: Government Document Book
Language:English
Published: Hampton, Va. : Hanover, MD : National Aeronautics and Space Administration, Langley Research Center ; Available from NASA Center for AeroSpace Information (CASI), [2001]
Series:NASA technical memorandum ; 210828.
Subjects:
Transonic wind tunnels.
Aerodynamic characteristics.
Dynamic pressure.
Static pressure.
Viscous flow.
Wind tunnel tests.
Online Access:Adobe Acrobat Reader required
Description
Item Description:Shipping list number: 2002-0157-M.
Shipping List Date: 02/25/2002
Microform.
Physical Description:1 volume
Also 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.