Vibration Analysis of Cantilevered Curved Plates Using a New Cylindrical Shell Finite Element

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Report Number: AFFDL TR 68-150 p. 247-269
Author(s): Olson, Mervyn D., Lindberg, Garry M.
Corporate Author(s): National Aeronautical Establishment
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Pages: 23
Contract: None Given
DoD Project: None Given
Identifier: This paper is part of a conference proceedings. See AD0703685

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Provenance: Lockheed Martin Missiles & Fire Control

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