Column and plate compressive strengths of aircraft structural materials: 17S-T aluminum-alloy sheet
Description:
From Summary: "Column and plate compressive strengths of 17S-T aluminum-alloy sheet were determined both within and beyond the elastic range from tests of thin-strip columns and from local-instability tests of formed Z- and channel-section columns. These tests are part of an extensive research investigation to provide data on the structural strengths of various aircraft materials. Results are presented in the form of curves and charts that may be used in the design and analysis of aircraft stru…
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Date:
June 1945
Creator:
Heimerl, George J. & Roy, J. Albert
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department