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LEADER 02450cam a2200589Ia 4500

001 ocm24956817;

003 OCoLC;

005 20050622144227.0;

007 he bmb024bbca;

008 911216s1990 vaua bb f000 0 eng d;

037 a| N 90-24660b| NASA;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:102679;

100 1 a| Carden, Huey D.=| ^A432034;

245 10 a| Unique failure behavior of metal/composite aircraft structural components under crash type loads /c| Huey D. Carden.;

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

300 a| 29 p. :b| ill. ;c| 28 cm.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 102679;

500 a| Shipping list no.: 1991-0130-M.;

500 a| Cover title.;

500 a| "May 1990.";

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

530 a| Also available via Internet from the NTRS web site. Address as of 6/22/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900015344%5F1990015344.pdf; current access is available via PURL.;

504 a| Includes bibliographical references (p. 9-11).;

650 0 a| Airplanesx| Crashworthiness.=| ^A427893;

650 0 a| Airframesx| Testing.=| ^A188236;

650 0 a| Airplanesx| Materialsx| Testing.=| ^A409964;

650 0 a| Metalsx| Fracture.=| ^A89976;

650 0 a| Composite materialsx| Fracture.=| ^A51796;

650 7 a| Aircraft accidents.2| nasat;

650 7 a| Composite structures.2| nasat;

650 7 a| Dynamic structural analysis.2| nasat;

650 7 a| Failure modes.2| nasat;

650 7 a| Impact damage.2| nasat;

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

650 7 a| Models.2| nasat;

650 7 a| Substructures.2| nasat;

650 7 a| Trends.2| nasat;

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

830 0 a| NASA technical memorandumv| 102679.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS61085;

949 a| NAS 1.15:102679w| sudoch| joyner32;

596 a| 1;

998 a| 1001391;

999 a| NAS 1.15:102679w| SUDOCc| 1i| MQ1765038d| 8/7/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 7/11/2005x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Unique failure behavior of metal/composite aircraft structural components under crash type loads / Huey D. Carden.

Author/creator	Carden, Huey D.
Other author	Langley Research Center.
Format	Microform
Publication Info	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990]
Description	29 p. : ill. ; 28 cm.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS61085
Subjects	Airplanes--Crashworthiness. Airframes--Testing. Airplanes--Materials. --Testing. Metals--Fracture. Composite materials--Fracture.

Series	NASA technical memorandum ; 102679 NASA technical memorandum 102679. ^A467613
General note	Shipping list no.: 1991-0130-M.
General note	Cover title.
General note	"May 1990."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 9-11).
Other forms	Also available via Internet from the NTRS web site. Address as of 6/22/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900015344%5F1990015344.pdf; current access is 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 1.15:102679
Stock number	N 90-24660 NASA

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:102679	✔ Available

Unique failure behavior of metal/composite aircraft structural components under crash type loads / Huey D. Carden.

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