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001 ocn232108730;

003 OCoLC;

005 20080616092012.0;

007 he bmb024b|ca;

008 080616s1984 vau b f000 0 eng d;

037 a| N 84-20650b| NASA;

040 a| GPOc| GPOd| MvI;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:85756;

100 1 a| Williams, Jerry G.=| ^A754747;

245 10 a| Effect of impact damage and open holes on the compression strength of tough resin/high strain fiber laminates /c| Jerry G. Williams.;

260 a| Hampton, Va. :b| National Aeronautics and Space Administration, Langley Research Center,c| [1984];

300 a| 1 v.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 85756;

530 a| Also available via Internet from the NTRS web site. Address as of 06/13/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19840012582%5F1984012582.pdf ; current access is available via PURL.;

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

650 0 a| Airplanesx| Design and construction.=| ^A75244;

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

650 0 a| Composite materialsx| Compression testing.=| ^A51796;

650 7 a| Compressive strength.2| nasat;

650 7 a| Graphite-epoxy composites.2| nasat;

650 7 a| Impact damages.2| nasat;

650 7 a| Impact tolerances.2| nasat;

650 7 a| Openings.2| nasat;

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

830 0 a| NASA technical memorandumv| 85756.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS95394;

949 a| NAS 1.15:85756w| sudoch| joyner32;

596 a| 1;

998 a| 1389738;

999 a| NAS 1.15:85756w| SUDOCc| 1i| MQ2550648l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 7/15/2008x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Effect of impact damage and open holes on the compression strength of tough resin/high strain fiber laminates / Jerry G. Williams.

Author/creator	Williams, Jerry G.
Other author	Langley Research Center.
Format	Microform
Publication Info	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1984]
Description	1 v.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS95394
Subjects	Airplanes--Design and construction. Composite materials--Delamination. Composite materials--Compression testing.

Series	NASA technical memorandum ; 85756 NASA technical memorandum 85756. ^A467613
General note	GPO Cataloging Record Distribution Program (CRDP).
Other forms	Also available via Internet from the NTRS web site. Address as of 06/13/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19840012582%5F1984012582.pdf ; current access is available via PURL.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1984. 1 microfiche.
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:85756
Stock number	N 84-20650 NASA

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:85756	✔ Available

Effect of impact damage and open holes on the compression strength of tough resin/high strain fiber laminates / Jerry G. Williams.

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