Flutter sensitivity to boundary layer thickness, structural damping, and static pressure differential for a shuttle tile overlay repair concept / 2009-215708

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Bibliographic Details
Author / Creator:Scott, Robert C.
Imprint:Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2009]
Description:1 online resource (30 pages) : illustrations (some color).
Language:English
Series:NASA/TM ; 2009-215708
NASA technical memorandum ; 2009-215708.
Subject:Aeroelasticity.
Boundary layers.
Computational fluid dynamics.
Dynamic structural analysis.
Space shuttles.
Structural vibration.
Tiles.
Vibration damping.
Format: E-Resource U.S. Federal Government Document Book
URL for this record:http://pi.lib.uchicago.edu/1001/cat/bib/8129372
Hidden Bibliographic Details
Other authors / contributors:Bartels, Robert E.
Langley Research Center.
Notes:Title from PDF title screen (viewed Aug. 6, 2010).
"April 2009."
Includes bibliographical references (pages 21-22).
GPO item no.:0830-D (online)
Govt.docs classification:NAS 1.15:2009-215708