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001 ocm57137031;

003 OCoLC;

005 20050505140019.0;

007 he bmb024b|ca;

008 041202s1991 caud bb f000 0 eng d;

037 a| N 91-17433b| NASA;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:101732;

100 1 a| Ko, William L.=| ^A420454;

245 10 a| Thermal behavior of a titanium honeycomb-core sandwich panel /c| William L. Ko and Raymond H. Jackson.;

300 a| 13 p. :b| charts ;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| 101732;

500 a| Distributed to depository libraries in microfiche.;

500 a| "January 1991.";

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

530 a| Also available via Internet from the NTRS web site. Address as of 5/5/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910008120%5F1991008120.pdf; current access is available via PURL.;

504 a| Includes bibliographical references (p. 6).;

650 0 a| Aerodynamic heating.=| ^A420455;

650 0 a| Airframes.=| ^A188236;

650 0 a| Titanium.=| ^A87677;

650 7 a| Finite element method.2| nasat;

650 7 a| Honeycomb cores.2| nasat;

650 7 a| Stress analysis.2| nasat;

650 7 a| Temperature effects.2| nasat;

650 7 a| Thermal stresses.2| nasat;

650 7 a| Titanium.2| nasat;

700 1 a| Jackson, Raymond H.=| ^A441211;

710 2 a| Dryden Flight Research Facility.=| ^A424598;

830 0 a| NASA technical memorandumv| 101732.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS60262;

949 a| NAS 1.15:101732w| sudoch| joyner32;

596 a| 1;

998 a| 999844;

999 a| NAS 1.15:101732w| SUDOCc| 1i| MQ1763473d| 8/7/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 6/24/2005x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Thermal behavior of a titanium honeycomb-core sandwich panel / William L. Ko and Raymond H. Jackson.

Author/creator	Ko, William L.
Other author	Jackson, Raymond H.
Other author	Dryden Flight Research Facility.
Format	Microform
Publication Info	Edwards, Calif. : NASA Ames Research Center, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor], 1991.
Description	13 p. : charts ; 28 cm.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS60262
Subjects	Aerodynamic heating. Airframes. Titanium.

Series	NASA technical memorandum ; 101732 NASA technical memorandum 101732. ^A467613
General note	Distributed to depository libraries in microfiche.
General note	"January 1991."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 6).
Other forms	Also available via Internet from the NTRS web site. Address as of 5/5/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910008120%5F1991008120.pdf; current access is available via PURL.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1991. 1 microfiche.
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:101732
Stock number	N 91-17433 NASA

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:101732	✔ Available

Thermal behavior of a titanium honeycomb-core sandwich panel / William L. Ko and Raymond H. Jackson.

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