Column and plate compressive strengths of aircraft structural materials. : Extruded 75S-T aluminum alloy / by George J. Heimerl and J. Albert Roy.
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| Corporate Authors: | , |
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| Other title: | NACA Wartime Reports. Series L. |
| Format: | Government Document Book |
| 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. L173. |
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| Abstract: | Column and plate compressive strengths of extruded 75S-T aluminum alloy were determined both within and beyond the elastic range from tests of thin-strip columns and local-instability tests of H-, Z-, and channel-section columns. These tests are part of an extensive research investigation to provide data on the structural strength of various aircraft materials. The results, which are presented in the form of curve and charts that are suitable for use in the design and analysis of aircraft structures, supersede preliminary results published previously. |
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| Item Description: | NACA Wartime Report L-173. Originally issued as NACA as Advance Restricted Report L5F08a (July 1945) Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. |
| Physical Description: | 11 pages, 12 unnumbered pages : illustrations ; 27 cm. |
| Bibliography: | Includes bibliographical references. |