Effect of Degradation of Material Properties on the Dynamic Response of Large Space Structures
Author:
Affiliation:
1. Texas A&M University, College Station, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.55558
Reference17 articles.
1. Minimum weight design of cylindrical shell with multiple stiffener sizes
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. On Thermally-Induced Vibrations of Structures in Space;Aerospace Thermal Structures and Materials for a New Era;1995-01-01
2. A model for predicting damage dependent damping in laminated composites;Computers & Structures;1988-01
3. A MODEL FOR PREDICTING DAMAGE DEPENDENT DAMPING IN LAMINATED COMPOSITES;Computational Structural Mechanics & Fluid Dynamics;1988
4. Finite-element model for the thermoelastic analysis of large composite space structures;Journal of Spacecraft and Rockets;1987-09
5. Predicted dynamic response of a composite beam with history-dependent damage;Computers & Structures;1987-01
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