An improved component-mode representation
Author:
Affiliation:
1. Aerospace Corp., El Segundo, Calif.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1974-386
Reference19 articles.
1. Ultimate Strengths of Laminated Composites
2. A Method of Predicting the Nonlinear Behavior of Laminated Composites
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1. Damage detection of spent nuclear fuel canisters using frequency response functions;Annals of Nuclear Energy;2023-06
2. Development of test-analysis models for large space structures usingsubstructure representations;Journal of Spacecraft and Rockets;1991-03
3. Projection and assembly method for multibody component model reduction;Journal of Guidance, Control, and Dynamics;1990-09
4. PROJECTION AND ASSEMBLY METHOD FOR MULTIBODY COMPONENT MODEL REDUCTION;Guidance, Navigation and Control Conference;1990-08-17
5. Comparison of the Craig-Bampton and residual flexibility methods of substructure representation;Journal of Aircraft;1987-04
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