Application of Reissner’s Variational Principle to Cantilever Plate Deflection and Vibration Problems
Author:
Affiliation:
1. Defense Research Laboratory, The University of Texas, Austin, Tex.
2. The University of Texas, Austin, Tex.
3. Boeing Airplane Company, Wichita, Kan.
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Link
http://asmedigitalcollection.asme.org/appliedmechanics/article-pdf/29/1/127/5444576/127_1.pdf
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5. Exact bending solutions of orthotropic rectangular cantilever thin plates subjected to arbitrary loads;International Applied Mechanics;2011-06
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