Modal Substructuring of Geometrically Nonlinear Finite-Element Models
Author:
Affiliation:
1. Sandia National Laboratories, Albuquerque, New Mexico 87185
2. University of Wisconsin-Madison, Madison, Wisconsin 53706-1609
3. U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054036
Reference41 articles.
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4. Reduced-order models for nonlinear response prediction: Implicit condensation and expansion
5. ZuchowskiB. “Predictive Capability for Hypersonic Structural Response and Life Prediction: Phase II – Detailed Design of Hypersonic Cruise Vehicle Hot-Structure,” U.S. Air Force Research Lab. TR-2012-0280, Wright–Patterson AFB, OH, May 2012.
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