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Tests on Stiffened Circular Cylinders

Marshall Holt

出版	National Advisory Committee for Aeronautics, 1941
URL	http://books.google.com.hk/books?id=l_FItwAACAAJ&hl=&source=gbs_api

註釋

Compressive tests were made of two series of stiffened circular cylindrical shells under axal load. All the shells were 16 inches in diameter by 24 inches in length and were made of aluminum-alloy sheet curved to the proper radius and welded with one longitudinal weld. The ratios and diameter to thickness of shell wall in the two series of specimens were 258 and 572. Strains were measured with Huggenberger tensometers at a number of gage lines on the stiffeners and shell. The test results are discussed in the light of published information on the subject.