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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Main Authors: | , , |
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Corporate Author: | |
Format: | eBook |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1947.
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
no. 1347. |
Subjects: | |
ISBN: | 9781680156065 1680156063 |
Physical Description: | 1 online resource (27 pages, 9 unnumbered pages) : illustrations, tables |
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. |
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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 |