Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy [microform] / David S. Dawicke.

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Bibliographic Details
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Main Author:	Dawicke, D. S.
Corporate Author:	Langley Research Center
Format:	Government Document Microfilm Book
Language:	English
Published:	Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1997]
Series:	NASA contractor report ; NASA CR-201668.
Subjects:	Fatigue (Materials) Crack propagation. Aluminum alloys. Compression loads.

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Holdings details from Online
Call Number:	NAS 1.26:201668
NAS 1.26:201668	Available

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:201668
NAS 1.26:201668	Restricted Place a Hold