Sidewall Mach number distributions for the NASA Langley Transonic Dynamics Tunnel /

Sidewall Mach number distributions for the NASA Langley Transonic Dynamics Tunnel /

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Bibliographic Details
Author / Creator:Florance, James R.
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/TM ; 2001-211019
NASA technical memorandum ; 211019.
Subject:
Calibration.
Flow meters.
Pressure -- Measurement.
Transonic wind tunnels.
Turbulence.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6532125
Hidden Bibliographic Details
Other authors / contributors:Rivera, JoseĢ A.
Langley Research Center.
Notes:Available via Internet from the NASA web site. Address as of 3/3/03: http://techreports.larc.nasa.gov/ltrs/PDF/2001/tm/NASA-2001-tm211019.pdf ; current access is available via PURL.
GPO item no.:0830-D (MF)
0830-D (online)
Govt.docs classification:NAS 1.15:211019

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