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001 ocn994007818;

003 OCoLC;

005 20170815101723.0;

006 m o d f ;

007 cr b||||||||||;

008 170718e200210 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 1.15:211888;

088 a| ICOMP-2002-05;

088 a| AIAA-2002-3630;

100 1 a| Yungster, Shaye,e| author.=| ^A438742;

245 10 a| Multiple-cycle simulation of a pulse detonation engine ejector /c| S. Yungster, H.D. Perkins.;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Glenn Research Center,c| October 2002.;

300 a| 1 online resource (10 pages) :b| illustration.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| 2002-211888;

500 a| "October 2002.";

500 a| "Prepared for the 38th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002.";

500 a| "Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.;

504 a| Includes bibliographical references (pages 4-5).;

513 a| Technical memorandum.;

536 a| Sponsored by the National Aeronautics and Space Administrationd| DlJ-708-48-13-00d| E-13570;

588 a| Description based on online resource; title from PDF title page (NASA, viewed July 18, 2017).;

500 a| "ICOMP-2002-05.";

500 a| "AIAA-2002-3630.";

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

650 7 a| Detonable gas mixtures.2| nasat;

650 7 a| Ejectors.2| nasat;

650 7 a| Impulses.2| nasat;

650 7 a| Mass flow rate.2| nasat;

650 7 a| Pulsed detonation engine.2| nasat;

650 7 a| Shock waves.2| nasat;

700 1 a| Perkins, Hugh Douglas,e| author.=| ^A568952;

710 2 a| NASA Glenn Research Center.b| Institute for Computational Mechanics in Propulsion,e| issuing body.=| ^A457544;

776 08 i| Print version:t| Multiple-cycle simulation of a pulse detonation engine ejectorw| (OCoLC)58927188;

776 08 i| Microfiche version:a| Yungster, Shaye.t| Multiple-cycle simulation of a pulse detonation engine ejectorw| (OCoLC)56350949;

830 0 a| NASA technical memorandumv| 2002-211888.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/LPS53266;

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

596 a| 1;

998 a| 4731289;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4731289-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 8/11/2017x| EDOCUMENTz| JERESOURCE;

Multiple-cycle simulation of a pulse detonation engine ejector / S. Yungster, H.D. Perkins.

Author/creator	Yungster, Shaye author.
Other author	Perkins, Hugh Douglas, author.
Other author	NASA Glenn Research Center. Institute for Computational Mechanics in Propulsion, issuing body.
Format	Electronic
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
Description	1 online resource (10 pages) : illustration.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS53266

Series	NASA/TM ; 2002-211888 NASA technical memorandum 2002-211888. ^A467613
General note	"October 2002."
General note	"Prepared for the 38th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002."
General note	"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
General note	"ICOMP-2002-05."
General note	"AIAA-2002-3630."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (pages 4-5).
Report note	Technical memorandum.
Funding information	Sponsored by the National Aeronautics and Space Administration DlJ-708-48-13-00 E-13570
Source of description	Description based on online resource; title from PDF title page (NASA, viewed July 18, 2017).
Issued in other form	Print version: Multiple-cycle simulation of a pulse detonation engine ejector
Issued in other form	Microfiche version: Yungster, Shaye. Multiple-cycle simulation of a pulse detonation engine ejector
Technical rpt number	ICOMP-2002-05
Technical rpt number	AIAA-2002-3630
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:211888

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Multiple-cycle simulation of a pulse detonation engine ejector / S. Yungster, H.D. Perkins.

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