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Effect of aspect ratio on undamped torsional oscillations of a thin rectangular wing in supersonic flow
Document ID
19930082576
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Watkins, Charles E
Date Acquired
August 29, 2013
Publication Date
June 1, 1949
Report/Patent Number
NACA-TN-1895
Report Number: NACA-TN-1895
Accession Number
93R11866
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLUTTER - WINGS
WINGS, RECTANGULAR
EQUATIONS - FLOW - SOURCES & SINKS
MATHEMATICS - BOUNDARY VALUES
THEORIES - WINGS
WINGS - TORSION
EQUATIONS - FLOW - DOUBLETS
WINGS - ASPECT RATIO
WINGS - OSCILLATIONS
WINGS, THIN
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