Improved Thermal Stress Determination by Finite Element Methods
Author:
Affiliation:
1. Grumman Aerospace Corporation, Bethpage, N. Y
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49424
Reference8 articles.
1. Przemieniecki, J. S., Theory of Matrix Structural Analysis, McGraw-Hill, New York, 1968, pp.62-64.
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