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Effects of side-edge boundary conditions and transverse shear stiffnesses on the flutter of orthotropic panels in supersonic flowSide edge boundary condition and transverse shear stiffness effects on orthotropic panel flutter in supersonic flow
Document ID
19660010465
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Weidman, D. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TN-D-3302
Report Number: NASA-TN-D-3302
Accession Number
66N19754
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC FLOW
PANEL FLUTTER
BOUNDARY LAYER FLOW
ORTHOTROPIC MATERIAL
SHEAR STRENGTH

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