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Supersonic Flutter of a Plate Containing Many Bays in the Spanwise Direction


Cummings, Benjamin Edgar (1957) Supersonic Flutter of a Plate Containing Many Bays in the Spanwise Direction. Engineer's thesis, California Institute of Technology. doi:10.7907/M4GA-0651.


A special problem of panel flutter is considered by the method of Galerkin. The solution to the supersonic, non-steady potential equation is obtained by the approach of Garrick and Rubinow. Plate equations of motion are obtained by use of the Lagrange equations. Numerical solutions to the flutter determinant are presented for two cases.

Item Type:Thesis (Engineer's thesis)
Subject Keywords:(Aeronautical Engineering)
Degree Grantor:California Institute of Technology
Division:Engineering and Applied Science
Major Option:Aeronautics
Thesis Availability:Public (worldwide access)
Research Advisor(s):
  • Fung, Yuan-cheng
Thesis Committee:
  • Unknown, Unknown
Defense Date:1 January 1957
Non-Caltech Author Email:bigben167 (AT)
Record Number:CaltechETD:etd-07082004-143419
Persistent URL:
Default Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:2832
Deposited By: Imported from ETD-db
Deposited On:13 Jul 2004
Last Modified:15 Aug 2023 20:57

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PDF (Cummings_be_1957.pdf) - Final Version
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