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A modified-strip-analysis method for predicting wing flutter at subsonic to hypersonic speedsModified strip analysis method for predicting wing flutter at subsonic to hypersonic speeds
Document ID
19660026804
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Yates, E. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1964
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-54830
Report Number: NASA-TM-X-54830
Accession Number
66N36094
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC FORCE
WING LOADING
FLUTTER ANALYSIS

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