Methodology of blade unsteady pressure measurement in the NASA transonic flutter cascade /

Methodology of blade unsteady pressure measurement in the NASA transonic flutter cascade /

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Bibliographic Details
Imprint:[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2002]
Description:1 v.
Language:English
Series:NASA/TM ; 2002-211894
NASA technical memorandum ; 211894.
Subject:
Aerodynamics, Transonic.
Computer simulation.
Pressure -- Measurement.
Unsteady flow (Aerodynamics)
Wind tunnels.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/6542472
Hidden Bibliographic Details
Other authors / contributors:Lepicovsky, J.
NASA Glenn Research Center.
Notes:Available via Internet from the Glenn Research Center web site. Address as of 1/21/03: http://gltrs.grc.nasa.gov/reports/2002/TM-2002-211894.pdf; current access available via PURL.
GPO item no.:0830-D (MF)
0830-D (online)
Govt.docs classification:NAS 1.15:211894 NAS 1.15:2002-211894

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