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001 ocn846225982;

003 OCoLC;

005 20160802131408.0;

006 m o d f ;

007 cr b|||||a|a||;

008 130602e199612 ohua obt f000 0 eng d;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:107331;

100 1 a| Gotsis, Pascal K.,e| author.?| UNAUTHORIZED;

245 10 a| Prediction of composite laminate fracture :b| micromechanics and progressive fracture /c| P.K. Gotsis and C.C. Chamis, L. Minnetyan.;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Lewis Research Center,c| December 1996.;

300 a| 1 online resource (14 pages) :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 107331;

500 a| Title from title screen (viewed July 26, 2016).;

500 a| "December 1996.";

500 a| "Performing organization: National National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.;

500 a| GPO Cataloging Record Distribution Program (CRDP).;

504 a| Includes bibliographical references (page 7).;

536 a| Sponsored by the National Aeronautics and Space Administrationd| WU-505-63-5Bd| E-10456;

650 7 a| Glass fibers.2| nasat;

650 7 a| Graphite-epoxy composites.2| nasat;

650 7 a| Matrix materials.2| nasat;

650 7 a| Laminates.2| nasat;

650 7 a| Epoxy matrix composites.2| nasat;

650 7 a| Residual stress.2| nasat;

650 7 a| Stress-strain relationships.2| nasat;

650 7 a| GRAPHITE.2| nasat;

650 7 a| FIBER COMPOSITES.2| nasat;

650 7 a| COMPOSITE MATERIALS.2| nasat;

650 7 a| FRACTURE MECHANICS.2| nasat;

700 1 a| Chamis, C. C.q| (Christos C.),e| author.=| ^A367779;

700 1 a| Minnetyan, Levon,d| 1946-e| author.=| ^A1302978;

710 2 a| Lewis Research Center,e| issuing body.=| ^A367825;

710 1 a| United States.b| National Aeronautics and Space Administratione| sponsoring body.=| ^A5437;

776 08 i| Print version:a| Gotsis, P. K.t| Prediction of composite laminate fracturew| (OCoLC)38136354;

776 08 i| Microfiche version:a| Gotsis, P. K.t| Prediction of composite laminate fracturew| (OCoLC)39722477;

830 0 a| NASA technical memorandumv| 107331.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo70378;

949 a| Click on web addressw| asish| joyner94;

596 a| 1;

998 a| 4507280;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4507280-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 8/12/2016x| EDOCUMENTz| JERESOURCE;

Prediction of composite laminate fracture : micromechanics and progressive fracture / P.K. Gotsis and C.C. Chamis, L. Minnetyan.

Author/creator	Gotsis, Pascal K. author.
Format	Electronic
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, December 1996.
Description	1 online resource (14 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo70378

Other author/creator	Chamis, C. C. (Christos C.), author.
Other author/creator	Minnetyan, Levon, 1946- author.
Other author/creator	Lewis Research Center, issuing body.
Other author/creator	United States. National Aeronautics and Space Administration sponsoring body.
Series	NASA technical memorandum ; 107331 NASA technical memorandum 107331. ^A467613
General note	Title from title screen (viewed July 26, 2016).
General note	"December 1996."
General note	"Performing organization: National National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 7).
Funding information	Sponsored by the National Aeronautics and Space Administration WU-505-63-5B E-10456
Issued in other form	Print version: Gotsis, P. K. Prediction of composite laminate fracture
Issued in other form	Microfiche version: Gotsis, P. K. Prediction of composite laminate fracture
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:107331

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Prediction of composite laminate fracture : micromechanics and progressive fracture / P.K. Gotsis and C.C. Chamis, L. Minnetyan.

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