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003 OCoLC;

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008 920106s1990 vaua bb f000 0 eng d;

037 a| N90-20427b| NASA;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:102590;

100 1 a| Dawicke, D. S.=| ^A440371;

245 10 a| Through-the-thickness fatigue crack closure behavior in an aluminum alloy /c| D.S. Dawicke, J.C. Newman, Jr., and A.F. Grandt, Jr.;

300 a| 6 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| 102590;

500 a| Cover title.;

500 a| "January 1990.";

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

504 a| Includes bibliographical references (p. 5).;

530 a| Also available via Internet from the NASA Technical Report Server web site. Address as of 8/18/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011111%5F1990011111.pdf ; current access is available via PURL.;

650 0 a| Aluminum alloysx| Fatigue.=| ^A605243;

650 7 a| Aluminum alloys.2| nasat;

650 7 a| Crack closure.2| nasat;

650 7 a| Crack propagation.2| nasat;

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

650 7 a| Stress intensity factors.2| nasat;

650 7 a| Thickness.2| nasat;

700 1 a| Newman, J. C.=| ^A424410;

700 1 a| Grandt, A. F.q| (Alten F.),d| 1945-=| ^A605244;

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

830 0 a| NASA technical memorandumv| 102590.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS62877;

949 a| NAS 1.15:102590w| sudoch| joyner32;

596 a| 1;

998 a| 1010063;

999 a| NAS 1.15:102590w| SUDOCc| 1i| MQ1778512d| 8/7/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 9/21/2005x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Through-the-thickness fatigue crack closure behavior in an aluminum alloy / D.S. Dawicke, J.C. Newman, Jr., and A.F. Grandt, Jr.

Author/creator	Dawicke, D. S.
Other author	Newman, J. C.
Other author	Grandt, A. F. (Alten F.), 1945-
Other author	Langley Research Center.
Format	Microform
Publication Info	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
Description	6 p. : ill.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS62877
Subjects	Aluminum alloys--Fatigue.

Series	NASA technical memorandum ; 102590 NASA technical memorandum 102590. ^A467613
General note	Cover title.
General note	"January 1990."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 5).
Other forms	Also available via Internet from the NASA Technical Report Server web site. Address as of 8/18/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011111%5F1990011111.pdf ; current access is available via PURL.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:102590
Stock number	N90-20427 NASA

Through-the-thickness fatigue crack closure behavior in an aluminum alloy / D.S. Dawicke, J.C. Newman, Jr., and A.F. Grandt, Jr.

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