Tools

LEADER 02257cam a2200565Ka 4500

001 ocn166289316;

003 OCoLC;

005 20070911150248.0;

007 he bmb024b|ca;

008 070824s1985 vau b f000 0 eng d;

037 a| N 86-14314b| NASA;

040 a| GPOc| GPOd| GPOd| MvI;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:87603z| NAS 1.15:87063;

100 1 a| Waters, William Allen.?| UNAUTHORIZED;

245 10 a| Failure mechanisms of laminates transversely loaded by bolt push-through /c| William Allen Waters, Jr. and Jerry G. Williams.;

260 a| Hampton, Va. :b| National Aeronautics and Space Administration, Langley Research Center,c| [1985];

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| 87603;

530 a| Also available via Internet from the NTRS web site. Address as of 8/23/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860004844%5F1986004844.pdf ; current access is available via PURL.;

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

650 0 a| Bolted joints.=| ^A52879;

650 0 a| Airplanesx| Fuselage.=| ^A670339;

650 0 a| Airframesx| Fatigue.=| ^A489811;

650 7 a| Adhesive bonding.2| nasat;

650 7 a| Bolts.2| nasat;

650 7 a| Composite materials.2| nasat;

650 7 a| Failure modes.2| nasat;

650 7 a| Fuselages.2| nasat;

650 7 a| Interlayers.2| nasat;

650 7 a| Laminates.2| nasat;

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

650 7 a| Panels.2| nasat;

650 7 a| Stiffening.2| nasat;

650 7 a| Toughness.2| nasat;

650 7 a| Wing panels.2| nasat;

700 1 a| Williams, Jerry G.=| ^A754747;

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

830 0 a| NASA technical memorandumv| 87603.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS85281;

949 a| NAS 1.15:87603w| sudoch| joyner32;

596 a| 1;

998 a| 1269344;

999 a| NAS 1.15:87603w| SUDOCc| 1i| MQ2263636l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 10/17/2007x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Failure mechanisms of laminates transversely loaded by bolt push-through / William Allen Waters, Jr. and Jerry G. Williams.

Author/creator	Waters, William Allen
Other author	Williams, Jerry G.
Other author	Langley Research Center.
Format	Microform
Publication Info	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
Description	1 v.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS85281
Subjects	Bolted joints. Airplanes--Fuselage. Airframes--Fatigue.

Series	NASA technical memorandum ; 87603 NASA technical memorandum 87603. ^A467613
General note	GPO Cataloging Record Distribution Program (CRDP).
Other forms	Also available via Internet from the NTRS web site. Address as of 8/23/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860004844%5F1986004844.pdf ; current access is available via PURL.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 1 microfiche.
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:87603 NAS 1.15:87063
Stock number	N 86-14314 NASA

Availability

Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:87603	✔ Available

Failure mechanisms of laminates transversely loaded by bolt push-through / William Allen Waters, Jr. and Jerry G. Williams.

Click here for more information about this title

Availability