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EXPERIMENTAL INVESTIGATION AT MACH NUMBER 3.0 OF EFFECTS OF THERMAL STRESS AND BUCKLING ON FLUTTER CHARACTERISTICS OF FLAT SINGLE-BAY PANELS OF LENGTH-WIDTH RATIO 0.96Supersonic effects of thermal stress and buckling on flutter of flat panels
Document ID
19630000331
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Dixon, S. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1962
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-1485
Report Number: NASA-TN-D-1485
Accession Number
63N10205
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THERMAL STRESS
THERMAL BUCKLING
PANEL FLUTTER
SUPERSONIC FLUTTER

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