Deployment Simulation Using Absolute Nodal Coordinate Plate Element for Next-Generation Aerospace Structures
Author:
Affiliation:
1. Tohoku University, Sendai 980-8579, Japan
Funder
Japan Society for the Promotion of Science
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J056477
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