Nonlinear Behavior of Space Shuttle Superlightweight Liquid-Oxygen Tank Under Prelaunch Loads
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681-2199
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3517
Reference11 articles.
1. Modeling and Nonlinear Structural Analysis of a Large-Scale Launch Vehicle
2. An improved estimate for the error in the classical, linear theory of plate bending
3. Postbuckling behavior of longitudinally compressed orthotropic plates with three-dimensional flexibility
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