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State and development of flutter calculationThis report discusses the need for considering a wide variation in certain of the basic flutter parameters in conducting a flutter analysis. Conclusions are drawn stating that design charts or simple rules may be misleading. Due to inherent difficulties, dynamic model testing may also yield misleading results. The general flutter equations and various methods of solution are discussed. Of particular interest, curves are presented showing computational effort plotted against a number of degrees of freedom used in a flutter analysis.
Document ID
19930093933
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Teichmann, Alfred
Date Acquired
August 16, 2013
Publication Date
March 1, 1951
Report/Patent Number
NACA-TM-1297
Report Number: NACA-TM-1297
Accession Number
93R23259
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VIBRATION AND FLUTTER - WINGS AND AILERONS
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