Experiment and theory of supersonic flutter in panels - length/width and stress ratios to prevent flutter of various thicknesses at mach 3
APPLICATION OF TRANSTABILITY CONCEPT TO FLUTTER OF FINITE PANELS AND EXPERIMENTAL RESULTS
1963-09-01
Sonstige
Keine Angabe
Englisch
Flutter of thermally buckled finite element panels
AIAA | 1976
|Flight flutter results for flat rectangular panels
TIBKAT | 1962
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