Aerodynamic solution for high frequency oscillations in supersonic flight is applied to calculation of bending-torsion flutter speed and frequency, including effects of airfoil thickness and shape; expressions are valid at sufficiently high frequencies and arbitrary supersonic Mach numbers; numerical results presented show variation of flutter boundary with elastic and inertial properties of airfoil, flight conditions and airfoil thickness.
Supersonic flutter calculation using high-frequency aerodynamic theory
Israel J Technology
Israel Journal of Technology ; 2 , n 1
1964
6 pages
Aufsatz (Zeitschrift)
Englisch
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Applications of high-frequency aerodynamic theory to calculation of flutter at supersonic speeds
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