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LEADER 02461nam a2200565 i 4500

001 on1001296703;

003 OCoLC;

005 20171102094806.0;

006 m o d f ;

007 cr bn|||||||||;

008 170817e199812 vaua obt f000 0 eng c;

035 a| (Sirsi) o1001296703;

042 a| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:208975;

100 1 a| Newman, J. C.,e| author.=| ^A424410;

245 10 a| Methodology for predicting the onset of widespread fatigue damage in lap-splice joints /c| J.C. Newman, Jr. [and three others].;

264 1 a| Hampton, Virginia :b| National Aeronautics and Space Administration, Langley Research Center,c| December 1998.;

300 a| 1 online resource (15 pages) :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| 1998-208975;

500 a| "December 1998.";

500 a| "Performing organization: NASA Langley Research Center"--Report documentation page.;

500 a| CRDP Program record.;

504 a| Includes bibliographical references (pages 10-11).;

513 a| Technical memorandum.;

536 a| Sponsored by the National Aeronautics and Space Administrationd| WU 522-18-11-01d| L-17799;

588 a| Description based on online resource; title from PDF title page (NASA, viewed Aug. 17, 2017).;

650 7 a| Crack propagation.2| nasat;

650 7 a| Crack tips.2| nasat;

650 7 a| Airframes.2| nasat;

650 7 a| Stress analysis.2| nasat;

650 7 a| Lap joints.2| nasat;

650 7 a| Fuselages.2| nasat;

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

650 7 a| Fatigue tests.2| nasat;

650 7 a| Fatigue (Materials)2| nasat;

710 2 a| Langley Research Center,e| issuing body.=| ^A192893;

776 08 i| Print version:t| Methodology for predicting the onset of widespread fatigue damage in lap-splice jointsw| (OCoLC)45517821;

776 08 i| Microfiche version:t| Methodology for predicting the onset of widespread fatigue damage in lap-splice jointsw| (OCoLC)41469782;

830 0 a| NASA technical memorandumv| 1998-208975.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo83872;

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

596 a| 1;

998 a| 4751360;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4751360-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 9/14/2017x| EDOCUMENTz| JERESOURCE;

Methodology for predicting the onset of widespread fatigue damage in lap-splice joints / J.C. Newman, Jr. [and three others].

Author/creator	Newman, J. C. author.
Other author	Langley Research Center, issuing body.
Format	Electronic
Publication	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, December 1998.
Description	1 online resource (15 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo83872

Series	NASA/TM ; 1998-208975 NASA technical memorandum 1998-208975. ^A467613
General note	"December 1998."
General note	"Performing organization: NASA Langley Research Center"--Report documentation page.
General note	CRDP Program record.
Bibliography note	Includes bibliographical references (pages 10-11).
Report note	Technical memorandum.
Funding information	Sponsored by the National Aeronautics and Space Administration WU 522-18-11-01 L-17799
Source of description	Description based on online resource; title from PDF title page (NASA, viewed Aug. 17, 2017).
Issued in other form	Print version: Methodology for predicting the onset of widespread fatigue damage in lap-splice joints
Issued in other form	Microfiche version: Methodology for predicting the onset of widespread fatigue damage in lap-splice joints
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:208975

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Methodology for predicting the onset of widespread fatigue damage in lap-splice joints / J.C. Newman, Jr. [and three others].

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