Type of Document	Master's Thesis
Author	Hedgepeth, John Mills
URN	etd-11072012-040239
Title	Flutter of rectangular simply supported panels at high supersonic speeds
Degree	Master of Science
Department	Applied Mechanics
Advisory Committee	Advisor Name Title Frederick, Daniel Committee Chair Pardue, Louis A. Committee Member Pletta, Dan H. Committee Member Whittemore, John A. Committee Member
Keywords	Flutter (Aerodynamics)
Date of Defense	1957-03-05
Availability	restricted
Abstract The panel flutter analysis presented herein has been restricted to the problem of an isolated simply supported plate of uniform thickness. The same type of analysis can be applied, however, to other panel configurations. Clamped panels, integrally stiffened panels, arrays of panels, end others should be amenable to treatment by the model approach based on the static aerodynamic approximation.
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