Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel
By: David M. Schuster.
Contributors: Langley Research Center.
Series: [NASA technical memorandum] -- NASA/TM-2001-210828.; NASA technical memorandum -- 210828.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from NASA Center for AeroSpace Information (CASI)
Published: 2001
Place of publication: Hampton, Va; Hanover, MD
Language: eng
Format: Microform
Subjects: Transonic wind tunnels.; Aerodynamic characteristics.; Dynamic pressure.; Static pressure.; Viscous flow.; Wind tunnel tests.
Notes: Shipping list no.: 2002-0157-M.

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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2001?] 1 microfiche.