The Creep Deformation of Symmetrically Loaded Circular Cylindrical Shells
Author:
Affiliation:
1. Pratt & Whitney Aircraft, Middletown, Conn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.8819
Reference7 articles.
1. Ferri, A n t o n i o , Supersonic Flow Around Circular Cones at Angles of Attack, N A C A Report 1045, 1 9 5 1 .
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1. Inelastic Response of Thin Shells;Thin Shell Theory;1980
2. Design methods for structures operating at high temperature;Nuclear Engineering and Design;1972-04
3. On the creep analysis of pressurized circular cylindrical shells;International Journal of Non-Linear Mechanics;1971-06
4. Secondary Creep of a Cylindrical thin Shell Subject to Axisymmetric Loading;Journal of Mechanical Engineering Science;1966-06
5. Approximate equations of creep of thin shells;Journal of Applied Mathematics and Mechanics;1963
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