A Refined Quadrilateral Element for Analysis of Plate Bending

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Report Number: AFFDL TR 68-150 p. 399-440
Author(s): Clough, Ray W., Felippa, Carlos A.
Corporate Author(s): University of California, Berkeley; Boeing Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Pages: 42
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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