Elevated-temperature compressive stress-strain data for 24S-T3 aluminum-alloy sheet and comparisons with extruded 75S-T6 aluminum alloy /
William M. Roberts and George J. Heimerl.

Description

Main Author

Roberts, William M.

Related Names

United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1949.

Subjects

Heimerl, George J.
Strains and stresses.
Sheet-metal.
Aluminum alloys.

Summary

Results 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.

Note

NACA TN No. 1837.
"March 1949."

Physical Description

11 p. : ill. ; 27 cm.

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