Title page for ETD etd-11072012-040239


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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