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001 ocm25053261;

003 OCoLC;

005 20060301101400.0;

007 he bmb024bbca;

008 920106s1990 vaua bbt f000 0 eng c;

037 a| N 90-21126b| NASA;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:102591;

100 1 a| Salpekar, Satish A.q| (Satish Annaji),d| 1954-=| ^A437488;

245 10 a| Combined effect of matrix cracking and stress-free edge on delamination /c| S.A. Salpekar and T.K. O'Brien.;

300 a| 64 p. :b| ill.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 102591;

490 1 a| AVSCOM technical memorandum ;v| 90-B-002;

500 a| Cover title.;

500 a| Shipping list no.: 90-0860-M.;

500 a| "March 1990.";

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

530 a| Also available via Internet from the NASA Technical Report Server web site. Address as of 3/1/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011810%5F1990011810.pdf; current access available via PURL.;

504 a| Includes bibliographical references (p. 30-32).;

650 0 a| Composite materialsx| Delamination.=| ^A436034;

650 7 a| Crack initiation.2| nasat;

650 7 a| Delaminating.2| nasat;

650 7 a| Edge loading.2| nasat;

650 7 a| Finite element method.2| nasat;

650 7 a| Laminates.2| nasat;

650 7 a| Strain energy release rate.2| nasat;

700 1 a| O'Brien, T. Kevin.=| ^A430485;

710 2 a| Langley Research Center.=| ^A192893;

710 1 a| United States.b| Army Aviation Systems Command.=| ^A367889;

830 0 a| NASA technical memorandumv| 102591.=| ^A467613;

830 0 a| AVSCOM technical memorandum ;v| 90-B-002.=| ^A437489;

856 41 u| https://purl.fdlp.gov/GPO/LPS67326;

949 a| NAS 1.15:102591w| sudoch| joyner32;

596 a| 1;

998 a| 1033899;

999 a| NAS 1.15:102591w| SUDOCc| 1i| MQ1814077d| 8/7/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 4/24/2006x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Combined effect of matrix cracking and stress-free edge on delamination / S.A. Salpekar and T.K. O'Brien.

Author/creator	Salpekar, Satish A., 1954-
Other author	O'Brien, T. Kevin.
Other author	Langley Research Center.
Other author	United States. Army Aviation Systems Command.
Format	Microform
Publication Info	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [ St. Louis, MO] : US Army Aviation Systems Command, [1990]
Description	64 p. : ill.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS67326
Subjects	Composite materials--Delamination.

Series	NASA technical memorandum ; 102591 AVSCOM technical memorandum ; 90-B-002 NASA technical memorandum 102591. ^A467613 AVSCOM technical memorandum ; 90-B-002. ^A437489
General note	Cover title.
General note	Shipping list no.: 90-0860-M.
General note	"March 1990."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 30-32).
Other forms	Also available via Internet from the NASA Technical Report Server web site. Address as of 3/1/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011810%5F1990011810.pdf; current access available via PURL.
Reproduction note	Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990] 1 microfiche : negative ; 11 x 15 cm.
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:102591
Stock number	N 90-21126 NASA

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:102591	✔ Available

Combined effect of matrix cracking and stress-free edge on delamination / S.A. Salpekar and T.K. O'Brien.

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