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

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

Internet

https://purl.fdlp.gov/GPO/LPS125046

Available Online

Holdings details from Available Online
Call Number: NAS 1.15:2009-215708
 
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NAS 1.15:2009-215708 Available