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LEADER 02551cam a2200565 a 4500

001 ocm25053284;

003 OCoLC;

005 20141208174348.0;

007 he bmb024bbca;

008 920106s1990 vaua bbt f000 0 eng d;

035 a| (Sirsi) o25053284;

035 a| (OCoLC)25053284;

040 d| GPOd| DLCd| MvId| UtOrBLW;

049 a| ERE$;

074 a| 0830-D (MF);

086 0 a| NAS 1.15:102592;

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

245 10 a| Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load /c| S.A. Salpekar, I.S. Raju, and T.K. O'Brien.;

300 a| 49 pages :b| illustrations.;

336 a| text2| rdacontent;

337 a| microform2| rdamedia;

338 a| microfiche2| rdacarrier;

490 1 a| AVSCOM technical memorandum ;v| 90-B-003;

490 1 a| NASA technical memorandum ;v| 102592;

500 a| Cover title.;

500 a| Distributed to depository libraries in microfiche.;

500 a| "March 1990.";

504 a| Includes bibliographical references (p. 17-18).;

536 a| National Aeronautics and Space Administration; U.S. Army Aviation Systems Command.d| 505-63-01-05.;

650 0 a| Laminated materialsx| Stress corrosion.=| ^A61622;

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

650 7 a| Delaminating.2| nasat;

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

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

650 7 a| Glass fiber reinforced plastics.2| nasat;

650 7 a| Laminates.2| nasat;

650 7 a| Loads (Forces)2| nasat;

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

650 7 a| Stress analysis.2| nasat;

700 1 a| Raju, I. S.=| ^A437490;

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

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

710 1 a| United States.b| Army Aviation Research and Technology Activity.=| ^A435693;

830 0 a| NASA technical memorandumv| 102592.=| ^A467613;

830 0 a| AVSCOM technical memorandum ;v| 90-B-003.=| ^A437489;

596 a| 1;

998 a| 701412;

999 a| NAS 1.15:102592w| SUDOCc| 1i| MQ1313270d| 8/6/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 2/8/2000x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load / S.A. Salpekar, I.S. Raju, and T.K. O'Brien.

Author/creator	Salpekar, Satish A., 1954-
Format	Microform
Publication Info	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center : US Army Aviation Systems Command, Aviation R&T Activity ; [Springfield, Va.] : [National Technical Information Service, distributor], [1990]
Description	49 pages : illustrations.
Subjects	Laminated materials--Stress corrosion. Composite materials--Delamination.

Other author/creator	Raju, I. S.
Other author/creator	O'Brien, T. Kevin.
Other author/creator	Langley Research Center.
Other author/creator	United States. Army Aviation Research and Technology Activity.
Series	AVSCOM technical memorandum ; 90-B-003 NASA technical memorandum ; 102592 NASA technical memorandum 102592. ^A467613 AVSCOM technical memorandum ; 90-B-003. ^A437489
General note	Cover title.
General note	Distributed to depository libraries in microfiche.
General note	"March 1990."
Bibliography note	Includes bibliographical references (p. 17-18).
Reproduction note	Joyner- Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990] 1 microfiche : negative.
Funding information	National Aeronautics and Space Administration; U.S. Army Aviation Systems Command. 505-63-01-05.
GPO item number	0830-D (MF)
Govt. docs number	NAS 1.15:102592

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:102592	✔ Available

Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load / S.A. Salpekar, I.S. Raju, and T.K. O'Brien.

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