Improvements on the analysis of shells of revolution by the matrix displacement method.
Author:
Affiliation:
1. Texas A&M University, College Station, Texas
2. Massachusetts Institute of Technology, Cambridge, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3854
Reference11 articles.
1. Application of matrix displacement method to linear elastic analysisof shells of revolution.
2. Irons, B. M. II. and Draper, K. T. "Inadequacy of nod connections in a stiffness solution for plate bending/7AIAA 3,961(1965).
3. Comments on ''numerical analysis of unsymmetrical bending of shells of revolution.'
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