Tensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F (370 ̊to 480 ̊K)
by Dick M. Royster.

Description

Main Author

Royster, Dick M.

Related Names

United States. National Aeronautics and Space Administration.
Langley Research Center.

Language(s)

English

Published

Washington, D.C. : National Aeronautics and Space Administration ; [1969]

Subjects

Supersonic transport planes > Supersonic transport planes / Materials > Supersonic transport planes / Materials / Environmental testing.
Aluminum alloys > Aluminum alloys / Creep.
Aluminum alloys > Aluminum alloys / Ductility.

Note

Prepared at Langley Research Center.
"January 1969"--Cover.

Physical Description

42 p. : ill. ; 27 cm.

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