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Critical-stress of Thin-walled Cylinders

S. B. Batdorf

出版	National Advisory Committee for Aeronautics, 1947
URL	http://books.google.com.hk/books?id=TyJbzQEACAAJ&hl=&source=gbs_api

註釋

Empirical design curves are presented for the critical stress of thin-walled cylinders loaded in axial compression. These curves are plotted in terms of the nondimensional parameters of small-deflection theory and are compared with theoretical curves derived from buckling of cylinders with simply supported and clamped edges. An empirical equation is given for the buckling of cylinders having a length-radius ratio greater than about 0.75.