Modeling of Highly Flexible Structures
Author:
Affiliation:
1. University of Missouri–Columbia, Columbia, Missouri 65211
2. North Carolina A&T State University, Greensboro, North Carolina 27411
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3577
Reference9 articles.
1. Interaction between an inflated lenticular reflector and its rim support
2. The unfolding deployment of a shell parabolic reflector
3. The Deployment of Curved Closed Tubes
4. Geometrically nonlinear formulation for the curved shell elements
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1. Dynamic Modeling and Experimental Validating of Large Semi-Rigid Structures;Journal of Mechanics;2014-03-17
2. Geometrically nonlinear analysis of shell structures using a flat triangular shell finite element;Archives of Computational Methods in Engineering;2006-09
3. Modeling, Analysis and Testing of some Deployable/Inflatable Structures;45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference;2004-04-19
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