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Effects of differential pressure, thermal stress, and buckling on flutter of flat panels with length-width ratio of 2Effect of differential pressure, thermal stress, & buckling on flutter of panels with length-width ratio of two
Document ID
19640001992
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dixon, S. C. (NASA Langley Research Center Hampton, VA, United States)
Shore, C. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1963
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-2047
Report Number: NASA-TN-D-2047
Accession Number
64N11901
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BUCKLING
PANEL FLUTTER
PRESSURE EFFECT
THERMAL STRESS

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