Numerical Method for Dynamic Analysis of Two-Dimensional Bimodular Structures
Author:
Affiliation:
1. State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, 116024 Dalian, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051530
Reference34 articles.
1. Tibert, G. "Deployable Tensegrity Structures for Space Applications," Ph.D. Dissertation,Royal Institute of Technology, Stockholm, 2002.
2. Adler, A. L. "Finite Element Approaches for Static and Dynamic Analysis of Partially Wrinkled Membrane Structures," Ph.D. Dissertation,Univ. of Colorado, Boulder, CO, 2000.
3. Stress-strain relations for materials with different moduli in tension and compression
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