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