Boundary integral equations for recovery of design sensitivities in shape optimization
Author:
Affiliation:
1. General Motors Research Laboratories, Warren, Michigan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9938
Reference22 articles.
1. Automatic Finite Element Modeling for Use with Three-Dimensional Shape Optimization
2. Optimal arrangement of holes in a two-dimensional heat conductor by a special boundary integral method
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