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001 ocn889078029;

003 OCoLC;

005 20210820074229.0;

006 m o d f ;

007 cr c||||||||||;

008 140825m20132014ohua obt f000 0 eng c;

042 a| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:2013-217822/PT.1-2;

086 0 a| NAS 1.15:2014-217822/PT.3;

100 1 a| Myers, David E.c| (Engineer),e| author.?| UNAUTHORIZED;

245 10 a| Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel /c| David E. Myers, Evan J. Pineda [and four others].;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Glenn Research Center,c| 2013-2014.;

300 a| 1 online resource (3 volumes) :b| color illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| 2013-217822;

490 1 a| NASA/TM ;v| 2014-217822;

588 a| Description based on online resource, Volume 1, PDF version; title from cover (NASA, viewed August 19, 2021).;

504 a| Includes bibliographical references.;

505 0 a| pt. 1. 8-ply in-autoclave facesheets -- pt. 2. 6-ply in-autoclave facesheets -- pt. 3. 8-ply out-of-autoclave facesheets.;

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

536 a| Sponsored by the National Aeronautics and Space Administrationh| WBS 432938.11.01.03.02.01.06h| WBS 585777.08.50.66.22.10;

536 d| E-18570d| E-18570-1d| GRC-E-DAA-TN10075d| NNC12BA01Bd| NNC09BA02B;

650 0 a| Fibrous composites.=| ^A56905;

650 0 a| Finite element method.=| ^A49224;

650 0 a| Honeycomb structures.=| ^A424669;

650 7 a| Fibrous composites.2| fast0| (OCoLC)fst00923679;

650 7 a| Finite element method.2| fast0| (OCoLC)fst00924897;

650 7 a| Honeycomb structures.2| fast0| (OCoLC)fst00959975;

650 7 a| Ares 5 cargo launch vehicle.2| nasat;

650 7 a| Epoxy matrix composites.2| nasat;

650 7 a| Fiber composites.2| nasat;

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

650 7 a| Honeycomb structures.2| nasat;

650 7 a| Robustness (mathematics)2| nasat;

650 7 a| Sandwich structures.2| nasat;

655 7 a| Technical reports.2| fast0| (OCoLC)fst01941336;

655 7 a| Technical reports.2| lcgft;

700 1 a| Pineda, Evan J.,e| author.=| ^A1381831;

710 2 a| NASA Glenn Research Center,e| issuing body.=| ^A420740;

710 1 a| United States.b| National Aeronautics and Space Administratione| sponsoring body.=| ^A5437;

830 0 a| NASA technical memorandumv| 217822.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo51535;

949 a| Click on web addressw| asish| joyner94;

596 a| 1;

998 a| 3652418;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 3652418-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 10/22/2014x| EDOCUMENTz| JERESOURCE;

Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel / David E. Myers, Evan J. Pineda [and four others].

Author/creator	Myers, David E. author.
Other author	Pineda, Evan J., author.
Other author	NASA Glenn Research Center, issuing body.
Other author	United States. National Aeronautics and Space Administration sponsoring body.
Format	Electronic
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2013-2014.
Description	1 online resource (3 volumes) : color illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo51535
Subjects	Fibrous composites. Finite element method. Honeycomb structures.

Series	NASA/TM ; 2013-217822 NASA/TM ; 2014-217822 NASA technical memorandum 217822. ^A467613
Contents	pt. 1. 8-ply in-autoclave facesheets -- pt. 2. 6-ply in-autoclave facesheets -- pt. 3. 8-ply out-of-autoclave facesheets.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references.
Funding information	Sponsored by the National Aeronautics and Space Administration WBS 432938.11.01.03.02.01.06 WBS 585777.08.50.66.22.10
Funding information	E-18570 E-18570-1 GRC-E-DAA-TN10075 NNC12BA01B NNC09BA02B
Source of description	Description based on online resource, Volume 1, PDF version; title from cover (NASA, viewed August 19, 2021).
Genre/form	Technical reports.
Genre/form	Technical reports.
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:2013-217822/PT.1-2
Govt. docs number	NAS 1.15:2014-217822/PT.3

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Buckling testing and analysis of honeycomb sandwich panel arc segments of a full-scale fairing barrel / David E. Myers, Evan J. Pineda [and four others].

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