Papers Published
Abstract:
An understanding of transonic flutter is often critical for high-speed aircraft development. A presentation of the transonic flutter velocity as a function of the Mach number and mass ratio is shown here to provide many advantages. Such a presentation offers new insights when comparing computational and wind-tunnel flutter results. The benefits of such a presentation are also evident in parameter studies. Finally, the subject of flutter similarity rules for airfoils of different thicknesses is also addressed.
Keywords:
Transonic aerodynamics;Airfoils;Velocity control;Thickness measurement;Degrees of freedom (mechanics);Frequencies;Pressure effects;Trajectories;Calculations;
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