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

Bibliographic Details
Main Author:	Scott, Robert C.
Corporate Author:	Langley Research Center
Other Authors:	Bartels, Robert E.
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2009]
Series:	NASA technical memorandum ; 2009-215708.
Subjects:	Aeroelasticity. Boundary layers. Computational fluid dynamics. Dynamic structural analysis. Space shuttles. Structural vibration. Tiles. Vibration damping.
Online Access:	https://purl.fdlp.gov/GPO/LPS125046

Description
Item Description:	Title from PDF title screen (viewed Aug. 6, 2010). "April 2009." Electronic resource.
Physical Description:	1 online resource (30 pages) : illustrations (some color).
Bibliography:	Includes bibliographical references (pages 21-22).