Tools

LEADER 01963cam 2200445Ia 4500

001 ocm46708464;

003 OCoLC;

005 20040909160053.0;

007 he bmb024bbca;

008 010411s1997 vaua bb f000 0 eng d;

040 a| EEXc| EEXd| GPOd| MvI;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:110309;

100 1 a| Rouse, Marshall.=| ^A432750;

245 10 a| Evaluation of a composite sandwich fuselage side panel with damage and subjected to internal pressure /c| Marshall Rouse ... [et al.].;

300 a| 18 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| 110309;

500 a| Cover title.;

500 a| Shipping list no.: 1997-0768-M.;

500 a| "February 1997.";

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

530 a| Also available via Internet from the NASA Web site. Address as of 9/09/04: http://techreports.larc.nasa.gov/ltrs/PDF/1997/tm/NASA-97-tm110309.pdf; current access available via PURL.;

504 a| Includes bibliographical references (p. 8).;

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

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

650 0 a| Airframesx| Design and construction.=| ^A989992;

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

830 0 a| NASA technical memorandumv| 110309.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS53294;

949 a| NAS 1.15:110309w| sudoch| joyner32;

596 a| 1;

998 a| 975353;

999 a| NAS 1.15:110309w| SUDOCc| 1i| MQ1724870d| 8/7/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 10/25/2004x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Evaluation of a composite sandwich fuselage side panel with damage and subjected to internal pressure / Marshall Rouse ... [et al.].

Author/creator	Rouse, Marshall
Other author	Langley Research Center.
Format	Microform
Publication Info	Hampton, Va. : Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
Description	18 p. : ill.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS53294
Subjects	Composite materials--Research. Airplanes--Fuselage. --Testing. Airframes--Design and construction.

Series	NASA technical memorandum ; 110309 NASA technical memorandum 110309. ^A467613
General note	Cover title.
General note	Shipping list no.: 1997-0768-M.
General note	"February 1997."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 8).
Other forms	Also available via Internet from the NASA Web site. Address as of 9/09/04: http://techreports.larc.nasa.gov/ltrs/PDF/1997/tm/NASA-97-tm110309.pdf; current access available via PURL.
Reproduction note	Microfiche. [Washington, D.C.] : NASA ; SuptDocs/GPO, 1997. 1 microfiche : negative.
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:110309

Evaluation of a composite sandwich fuselage side panel with damage and subjected to internal pressure / Marshall Rouse ... [et al.].

Click here for more information about this title