Fatigue life methodology for bonded composite skin/stringer configurations /

Fatigue life methodology for bonded composite skin/stringer configurations /

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Bibliographic Details
Imprint:	Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, 2001.
Description:	40 p. : ill. ; 28 cm.
Language:	English
Series:	NASA TM- ; 2001-210842 NASA technical memorandum ; 2001-210842.
Subject:	Composite materials. Fracture mechanics. Materials -- Fatigue. Composite materials. Fracture mechanics. Materials -- Fatigue.
Format:	U.S. Federal Government Document Print Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/4488793

Hidden Bibliographic Details
Other authors / contributors:	Krueger, Ronald. U.S. Army Research Laboratory. Langley Research Center.
Notes:	"April 2001." "Performing organization report number L-18067"--Report documentation page. Includes bibliographical references. Performed by U.S. Army Research Laboratory for Langley Research Center. WU 712-10-21-01

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Call Number:	TA418.9.C6F385 2001
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