Development and Evaluation of Solution Procedures for Geometrically Nonlinear Structural Analysis
Author:
Affiliation:
1. Texas A & M University, College Station, Texas
2. Manned Spacecraft Center, Houston, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50089
Reference36 articles.
1. Large Deflections of Structures Subjected to Heating and External Loads
2. Finite asymmetric deformation of shallow spherical shells
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