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Modified-strip-analysis method for predicting wing flutter at subsonic to hypersonic speeds.Modified strip analysis method for predicting finite-span, swept or unswept wing flutter at subsonic to hypersonic speeds
Document ID
19660041448
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Yates, E. C., Jr.
Date Acquired
August 3, 2013
Publication Date
February 1, 1966
Subject Category
Aerodynamics
Accession Number
66A20738
Distribution Limits
Public
Copyright
Other
Keywords
FLUTTER ANALYSIS
OSCILLATING WING
AERODYNAMIC LOAD

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