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001 ocm25699100;

003 OCoLC;

005 20060301092713.0;

007 he bmb024bbca;

008 920423s1990 vaua bbt f000 0 eng c;

037 a| N 90-21424b| NASA;

042 a| pcc;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:101675;

245 03 a| An evaluation of the pressure proof test concept for thin sheet 2024-T3 /c| D.S. Dawicke ... [et al.].;

260 a| Hampton, Va. :b| National Aeronautics and Space Administration, Langley Research Center,c| [1990];

300 a| 30 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| 101675;

500 a| Cover title.;

500 a| Shipping list no.: 90-0857-M.;

500 a| "April 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/19900012108%5F1990012108.pdf; current access available via PURL.;

504 a| Includes bibliographical references (p. 14-15).;

536 h| 505-63-01-05;

650 0 a| Airplanesx| Fuselagex| Testing.=| ^A670339;

650 7 a| Crack propagation.2| nasat;

650 7 a| Cracks.2| nasat;

650 7 a| Fatigue life.2| nasat;

650 7 a| Fracture mechanics.2| nasat;

650 7 a| Fuselages.2| nasat;

650 7 a| Structural failure.2| nasat;

650 7 a| Transport aircraft.2| nasat;

700 1 a| Dawicke, D. S.=| ^A440371;

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

830 0 a| NASA technical memorandumv| 101675.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS67255;

949 a| NAS 1.15:101675w| sudoch| joyner32;

596 a| 1;

998 a| 1033930;

999 a| NAS 1.15:101675w| SUDOCc| 1i| MQ1814108d| 8/7/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 4/24/2006x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

An evaluation of the pressure proof test concept for thin sheet 2024-T3 / D.S. Dawicke ... [et al.].

Other author	Dawicke, D. S.
Other author	Langley Research Center.
Format	Microform
Publication Info	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
Description	30 p. : ill.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS67255
Subjects	Airplanes--Fuselage. --Testing.

Series	NASA technical memorandum ; 101675 NASA technical memorandum 101675. ^A467613
General note	Cover title.
General note	Shipping list no.: 90-0857-M.
General note	"April 1990."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 14-15).
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/19900012108%5F1990012108.pdf; current access available via PURL.
Reproduction note	Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990] 1 microfiche : negative.
Funding information	505-63-01-05
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:101675
Stock number	N 90-21424 NASA

An evaluation of the pressure proof test concept for thin sheet 2024-T3 / D.S. Dawicke ... [et al.].

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