Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material

Fracture test results for 0.5, 0.7 and 0.9 in ...
William M. Johnston
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Last edited by WorkBot
January 17, 2010 | History

Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material

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Edition Availability
Cover of: Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material
Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material
2001, National Aeronautics and Science Administration, Langley Research Center, Available from NASA Center for Aerospace Information
Microform in English
Cover of: Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material
Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material
2001, National Aeronautics and Science Administration, Langley Research Center, Available from NASA Center for Aerospace Information
Microform in English

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Book Details


Edition Notes

Shipping list no.: 2002-0173-M.

"March 2001."

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?] 1 microfiche.

Published in
Hampton, Va, Hanover, MD
Series
[NASA contractor report] -- NASA/CR-2001-210833., NASA contractor report -- NASA CR-210833.

The Physical Object

Format
Microform
Pagination
1 v.

Edition Identifiers

Open Library
OL17607397M
OCLC/WorldCat
50134450

Work Identifiers

Work ID
OL10436605W

Source records

Oregon Libraries MARC record

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January 17, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page