Attempt made to correlate theoretically calculated decay effects of wing oscillations at subcritical flutter speeds with results obtained during actual flight flutter testing at these speeds; theory discussed gives reasonably good agreement with limited number of test data obtained in flight from single airplane.
Note on flight flutter testing
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 15 , n 6
1948
5 pages
Aufsatz (Zeitschrift)
Englisch
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NTIS | 1992
|Flight Flutter Testing Symposium
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AIAA | 1975
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|Flight Flutter Testing Symposium
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