Flutter boundaries obtained from experiments are compared with various theoretical predictions; modal analysis of Donnell's equations is used in conjunction with piston theory and potential solution of R.W.Leonard and J.M.Hedgepeth; it was found that pressurized cylindrical shells fluttered at lower level of freestream energy than predicted by either theory; of two results, that using piston theory appears to correspond more closely to experiment.
Comparing theory and experiment for supersonic flutter of circular cylindrical shells
AIAA J
AIAA Journal ; 5 , n 10
1967
8 pages
Aufsatz (Zeitschrift)
Englisch
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