Critical combinations of shear and longitudinal direct stress for long plates with transverse curvature

A theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a compari...

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Bibliographic Details
Main Authors: Batdorf, S. B., (Author), Schildcrout, Murry, (Author), Stein, Manuel, (Author)
Corporate Author: Langley Aeronautical Laboratory.
Format: eBook
Language: English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Series: Technical note (United States. National Advisory Committee for Aeronautics) ; no. 1347.
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ISBN: 9781680156065
1680156063
Physical Description: 1 online resource (27 pages, 9 unnumbered pages) : illustrations, tables

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Summary: A theoretical solution is presented for the buckling stresses of long plates with transverse curvature loaded in shear and longitudinal direct stress. The theoretical critical-stress combinations for plates having either simply supported or clamped edges are given in figures and tables and a comparison is made with a previous theoretical solution for simply supported plates.
Item Description: "Langley Memorial Aeronautical Laboratory."
Date of issue: June 1947.
Report no. NACA TN No. 1347.
Bibliography: Includes bibliographical references (pages 23-24)
ISBN: 9781680156065
1680156063
Access: Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty