Elevated-temperature compressive stress-strain data for 24S-T3 aluminum-alloy sheet and comparisons with extruded 75S-T6 aluminum alloy

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100 1 ⊔ ‡aRoberts, William M.
245 1 0 ‡aElevated-temperature compressive stress-strain data for 24S-T3 aluminum-alloy sheet and comparisons with extruded 75S-T6 aluminum alloy / ‡cWilliam M. Roberts and George J. Heimerl.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c1949.
300 ⊔ ⊔ ‡a11 p. : ‡bill. ; ‡c27 cm.
490 0 ⊔ ‡aNational Advisory Committee for Aeronautics ; ‡vno. 1837
500 ⊔ ⊔ ‡aNACA TN No. 1837.
500 ⊔ ⊔ ‡a"March 1949."
504 ⊔ ⊔ ‡aIncludes bibliographical references.
520 3 ⊔ ‡aResults are presented of compressive stress-strain tests of 24S-T3 aluminum-alloy sheet at stabilized elevated temperatures up to 700 degrees F, exposure times of 1/2 to 2 hours, and strain rates of 0.002 to 0.006 per minute. Some general comparisons with extruded 75S-T6 aluminum alloy are included.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aHeimerl, George J.
650 ⊔ 0 ‡aStrains and stresses.
650 ⊔ 0 ‡aSheet-metal.
650 ⊔ 0 ‡aAluminum alloys.
710 1 ⊔ ‡aUnited States. ‡bNational Advisory Committee for Aeronautics.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
899 ⊔ ⊔ ‡a39015086493619
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