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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.

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Format:
Book
Government document
Author/Creator:
Royster, Dick M., author.
Contributor:
United States. National Aeronautics and Space Administration, issuing body.
Series:
NASA technical note ; D-5010.
NASA/TN ; D-5010
Language:
English
Subjects (All):
Aluminum alloys--Ductility.
Aluminum alloys.
Aluminum alloys--Creep.
Supersonic transport planes--Materials--Environmental testing.
Supersonic transport planes.
Physical Description:
1 online resource (42 pages) : illustrations
Place of Publication:
Washington, D.C. : National Aeronautics and Space Administration, January 1969.
Notes:
"January 1969."
Includes bibliographical references (page 12).
Online resource, PDF version; title from title page (NASA, viewed on May 12, 2021).
Other Format:
Print version: Royster, Dick M. Tensile properties and creep strength of three aluminum alloys exposed up to 25,000 hours at 200 ̊to 400 ̊F (370 ̊to 480 ̊K).
OCLC:
785108102

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