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

Description
Physical Description:	1 v.
Format:	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.