Critical-stress of thin-walled cylinders in axial compression

• Main Authors: Batdorf, S. B. (Author), Schildcrout, Murry (Author), Stein, Manuel (Author)
• Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
• Format: Electronic eBook
• Language: English
• Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
• Series: Technical note (United States. National Advisory Committee for Aeronautics) ; 1343.
• Subjects: Thin-walled structures.; Cylinders.; Strains and stresses.; elektronické knihy; electronic books
• ISBN: 9781680156119; 168015611X
• Physical Description: 1 online resource (17 pages) : illustrations
• Item Description: "Langley Memorial Aeronautical Laboratory."; Date of issue: June 1947.; Report no. NACA-TN-1343.
• Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty

Empirical design curves are presented for the critical stress of thin-walled cylinders loaded in axial compression. These curves are plotted in terms of nondimensional parameters of small-deflection theory and are compared with theoretical curves derived for the 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. The test data obtained from various sources follow the general trend of the theoretical curve for cylinders with clamped edges, agreeing closely with the theory in the case of short cylinders, but falling considerably below the theoretical results for long cylinders. --