Publications [#281328] of Kenneth C. Hall
- Kholodar, DB; Dowell, EH; Thomas, JP; Hall, KC, Improved understanding of transonic flutter: A three-parameter flutter surface,
Journal of Aircraft, vol. 41 no. 4
pp. 911-917, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]
(last updated on 2020/07/16)
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.
Transonic aerodynamics;Airfoils;Velocity control;Thickness measurement;Degrees of freedom (mechanics);Frequencies;Pressure effects;Trajectories;Calculations;