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Experimental Study of the Effect of Length on the Buckle Pattern of Axially Compressed Circular Cylindrical Shells
R. L. Sendelbeck
Stanford University. Department of Aeronautics and Astronautics
R. L. Carlson
N. J. Hoff
出版
Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force
, 1967
URL
http://books.google.com.hk/books?id=J9ADAAAAIAAJ&hl=&source=gbs_api
註釋
Ten thin-walled circular cylindrical shells were tested in axial compression to observe the effect of the length-to-radius ratio on the buckling pattern. At an approximate value of 600 of the radius to thickness ratio the number of waves around the circumference was found, in a first approximation, to very inversely with the cube root of the length-to-radius ratio. (Author).
