Tools

LEADER 02336cam a2200529Ii 4500

001 ocn825550608;

003 OCoLC;

005 20130128091620.0;

006 m o d f ;

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

008 130128s2012 ohua obt f000 0 eng d;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:2012-217714;

100 1 a| Csank, Jeffrey T.,e| author.=| ^A1412441;

245 12 a| A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool /c| Jeffrey T. Csank and Thomas J. Stueber.;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Glenn Research Center,c| 2012.;

300 a| 1 online resource (13 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| 2012-217714;

500 a| Title from title screen (viewed on Jan. 14, 2013).;

500 a| "September 2012.";

500 a| "Prepared for the 48th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE Atlanta, Georgia, July 30 to August 1, 2012.";

504 a| Includes bibliographical references (pages 12-13).;

536 a| Sponsored by National Aeronautics and Space Administrationh| WBS 599489.02.07.03.07.11.02;

536 e| E-18419;

500 a| "AIAA-2012-4149.";

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

650 7 a| Computerized simulation.2| nasat;

650 7 a| Propulsion system configurations.2| nasat;

650 7 a| Wind tunnel tests.2| nasat;

650 7 a| Fuel systems.2| nasat;

650 7 a| Propulsion system performance.2| nasat;

650 7 a| Turbine engines.2| nasat;

650 7 a| Engine inlets.2| nasat;

700 1 a| Stueber, Thomas J.,e| author.=| ^A1419524;

710 2 a| NASA Glenn Research Centere| issuing body.=| ^A420740;

711 2 a| Joint Propulsion Conference and Exhibitn| (48th :d| 2012 :c| Atlanta, Ga.)=| ^A1134656;

830 0 a| NASA technical memorandumv| 2012-217714.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo33018;

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

596 a| 1;

998 a| 3281720;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 3281720-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 3/11/2013x| EDOCUMENTz| JERESOURCE;

A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool / Jeffrey T. Csank and Thomas J. Stueber.

Author/creator	Csank, Jeffrey T. author.
Other author	Stueber, Thomas J., author.
Other author	NASA Glenn Research Center issuing body.
Other author	Joint Propulsion Conference and Exhibit 2012 : Atlanta, Ga.)
Format	Electronic
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
Description	1 online resource (13 pages) : color illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo33018

Series	NASA/TM ; 2012-217714 NASA technical memorandum 2012-217714. ^A467613
General note	Title from title screen (viewed on Jan. 14, 2013).
General note	"September 2012."
General note	"Prepared for the 48th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE Atlanta, Georgia, July 30 to August 1, 2012."
General note	"AIAA-2012-4149."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (pages 12-13).
Funding information	Sponsored by National Aeronautics and Space Administration WBS 599489.02.07.03.07.11.02
Funding information	E-18419
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:2012-217714

Availability

Library	Location	Call Number	Status	Item Actions
	Electronic Resources	Access Content Online	✔ Available

A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool / Jeffrey T. Csank and Thomas J. Stueber.

Click here for more information about this title

Availability