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LEADER 02173cam 2200529 i 4500

001 ocn883215359;

003 OCoLC;

005 20140709114120.0;

006 m o d f ;

007 cr m||||||||||;

008 140709e201312 ohua obt f000 0 eng c;

040 a| GPOb| enge| rdae| pnc| GPOd| MvI;

042 a| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:2013-214029;

100 1 a| Hughes, Christopher E.,e| author.=| ^A441165;

245 14 a| The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator /c| Christopher E. Hughes [and three others].;

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

300 a| 1 online resource (35 pages) :b| illustrations (some color).;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| 2013-214029;

500 a| Title from title screen (viewed July 9, 2014).;

500 a| "December 2013.";

504 a| Includes bibliographical references (page 13).;

536 a| Sponsored by National Aeronautics and Space Administrationh| WBS-22-781-30-75;

536 d| E-15384;

500 a| "GT2005-68573.";

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

650 7 a| Aeroacoustics.2| nasat;

650 7 a| Aerodynamic characteristics.2| nasat;

650 7 a| Aerodynamic noise.2| nasat;

650 7 a| Aircraft noise.2| nasat;

650 7 a| Fan blades.2| nasat;

650 7 a| Far fields.2| nasat;

650 7 a| Laser doppler velocimeters.2| nasat;

650 7 a| Low speed wind tunnels.2| nasat;

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| 2013-214029.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo50531;

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

596 a| 1;

998 a| 3503685;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 3503685-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 8/12/2014x| EDOCUMENTz| JERESOURCE;

The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / Christopher E. Hughes [and three others].

Author/creator	Hughes, Christopher E. 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, December 2013.
Description	1 online resource (35 pages) : illustrations (some color).
Supplemental Content	https://purl.fdlp.gov/GPO/gpo50531

Series	NASA/TM ; 2013-214029 NASA technical memorandum 2013-214029. ^A467613
General note	Title from title screen (viewed July 9, 2014).
General note	"December 2013."
General note	"GT2005-68573."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 13).
Funding information	Sponsored by National Aeronautics and Space Administration WBS-22-781-30-75
Funding information	E-15384
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:2013-214029

The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / Christopher E. Hughes [and three others].

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