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Creep Buckling of Plates and Shells

Stanford University. Department of Aeronautics and AstronauticsNicholas J. Hoff

出版	Stanford University, Department of Aeronautics and Astronautics, 1972
URL	http://books.google.com.hk/books?id=JcgDAAAAIAAJ&hl=&source=gbs_api

註釋

A review is presented of the fundamental considerations that enter into the calculation of the buckling of plates and shells whose material deforms in consequence of nonlinear creep. Results are given of analyses that have been carried out for flat plates subjected to edge-wise compression and for circular cylindrical shells subjected to uniform axial compression, to a uniform external pressure and to a constant bending moment. The character of the behavior of these structural elements after buckling is also discussed. (Author).