Stability of transient solution of moderately thick plate by finite-difference method
Author:
Affiliation:
1. Army Materials and Mechanics Research Center, Watertown, Mass.
2. Massachusetts Institute of Technology, Cambridge, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6463
Reference3 articles.
1. Stability of Finite-Difference Equation for the Transient Response of a Flat Plate
2. Leech, J. W. "Finite-Difference Calculation Method for Large Elastic-Plastic Dynamically Induced Deformations of General Thin Shells/7AFFDL TR 66-171, Dec. 1964, Air Force Flight Dynamics Lab., Wright-Patterson Air Force Base, Ohio.
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