Effect of normal pressure on the critical compressive and shear stress of curved sheet /
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| Corporate Authors: | , , |
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| Format: | eBook |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1945]
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| Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. L57. |
| Subjects: | |
| Online Access: | Connect to the full text of this electronic book |
| Abstract: | Results are presented of tests of two sets of 20 curved-sheet specimens to determine the effect of normal pressure on the critical compressive and shear stress of curved sheet. It was found that normal pressure raised the critical compressive and shear stress of curved sheet except when outward bulging occurred in compression, in which case the critical stress was lowered by normal pressure. |
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| Item Description: | NACA Wartime Report L-57. Originally issued as NACA as Advance Restricted Report L5B10 (March 1945). Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. Electronic resource. |
| Physical Description: | 1 online resource (7 pages, 8 unnumbered pages) : illustrations. |
| Bibliography: | Includes bibliographical references. |
| ISBN: | 9781680156355 1680156357 |