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Single-degree-of-freedom-flutter calculations for a wing in subsonic potential flow and comparison with an experimentThe effect of Mach number and structural damping on single-degree-of-freedom pitching of a wing is presented. Some experimental results are compared with theory and good agreement is found for certain ranges of an inertia parameter.
Document ID
19930090966
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Runyan, Harry L
Date Acquired
September 6, 2013
Publication Date
January 1, 1952
Report/Patent Number
NACA-TR-1089
Report Number: NACA-TR-1089
Accession Number
93R20256
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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