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Book Cover
E-book
Author Batdorf, S. B., author.

Title Critical-stress of thin-walled cylinders in axial compression / by S.B. Batdorf, Murry Schildcrout, and Manuel Stein, Langley Memorial Aeronautical Laboratory, Langley Field, Va
Published Washington, D.C. : National Advisory Committee for Aeronautics, 1947

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Description 1 online resource (17 pages) : illustrations
Series Technical note ; no. 1343
Technical note (United States. National Advisory Committee for Aeronautics) ; 1343.
Summary 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. -- Provided by publisher
Notes "Langley Memorial Aeronautical Laboratory."
Date of issue: June 1947
Report no. NACA-TN-1343
Bibliography Includes bibliographical references (pages 15-16)
Notes digitized 2011 University of North Texas committed to preserve pda TXdn
Print version record
Subject Thin-walled structures.
Cylinders.
Strains and stresses.
cylinders (solids)
Thin-walled structures
Cylinders
Strains and stresses
Form Electronic book
Author Schildcrout, Murry, author
Stein, Manuel, author
United States. National Advisory Committee for Aeronautics.
Langley Aeronautical Laboratory.
ISBN 9781680156119
168015611X