Tools

LEADER 02224cam 2200481Ii 4500

001 ocn910116245;

003 OCoLC;

005 20150526162452.0;

006 m o d f ;

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

008 150526e201502 ohua obt f000 0 eng d;

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

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:2015-218475;

100 1 a| Tedder, Sarah A.,e| author.?| UNAUTHORIZED;

245 10 a| Fundamental study of a single point lean direct injector part I :b| effect of air swirler angle and injector tip location on spray characteristics /c| Sarah A. Tedder [and three others].;

246 30 a| Effect of air swirler angle and injector tip location on spray characteristics;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Glenn Research Center,c| February 2015.;

300 a| 1 online resource (14 pages) :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| 2015-218475;

500 a| Title from title screen (viewed on May 26, 2015).;

500 a| "February 2015.";

500 a| "Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, ASEE, Cleveland, Ohio, July 28-30, 2014.";

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

504 a| Includes bibliographical references (pages 13-14).;

536 a| Sponsored by the NASA Fundamental Aeronautics Programd| AIAA-2014-3435;

650 7 a| Turbulent mixing.2| nasat;

650 7 a| Turbulent combustion.2| nasat;

650 7 a| Fuel injection.2| nasat;

650 7 a| Recirculative fluid flow.2| nasat;

650 7 a| Computational fluid dynamics.2| nasat;

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

710 2 a| Fundamental Aeronautics Program (U.S.),e| sponsoring body.=| ^A1093481;

830 0 a| NASA technical memorandumv| 2015-218475.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo57559;

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

596 a| 1;

998 a| 3778845;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 3778845-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 7/16/2015x| EDOCUMENTz| JERESOURCE;

Fundamental study of a single point lean direct injector part I : effect of air swirler angle and injector tip location on spray characteristics / Sarah A. Tedder [and three others].

Author/creator	Tedder, Sarah A. author.
Other author	NASA Glenn Research Center, issuing body.
Other author	Fundamental Aeronautics Program (U.S.), sponsoring body.
Format	Electronic
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2015.
Description	1 online resource (14 pages) : color illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo57559

Portion of title	Effect of air swirler angle and injector tip location on spray characteristics
Series	NASA/TM ; 2015-218475 NASA technical memorandum 2015-218475. ^A467613
General note	Title from title screen (viewed on May 26, 2015).
General note	"February 2015."
General note	"Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, ASEE, Cleveland, Ohio, July 28-30, 2014."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (pages 13-14).
Funding information	Sponsored by the NASA Fundamental Aeronautics Program AIAA-2014-3435
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:2015-218475

Fundamental study of a single point lean direct injector part I : effect of air swirler angle and injector tip location on spray characteristics / Sarah A. Tedder [and three others].

Click here for more information about this title