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

042 a| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:210679;

100 1 a| Steffen, Christopher J.,e| author.=| ^A573756;

245 10 a| Computational analysis of the combustion process in an axisymmetric,RBCC flowpath /c| Christopher J. Steffen, Shaye Yungster.;

246 3 a| Computational analysis of the combustion processes in an axisymmetric, rocket based combined cycle flowpath;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Glenn Research Center,c| February 2001.;

300 a| 1 online resource (15 pages) :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| 2001-210679;

500 a| "February 2001.";

500 a| "Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting cosponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000.";

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

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

504 a| Includes bibliographical references (page 15).;

513 a| Technical memorandum.;

536 a| Sponsored by the National Aeronautics and Space Administrationd| WU-708-65-13-00 d E-12606;

588 a| Description based on online resource; title from PDF title page (NASA, viewed Nov. 20, 2017).;

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

650 7 a| Numerical analysis.2| nasat;

650 7 a| Combustion physics.2| nasat;

650 7 a| Three dimensional models.2| nasat;

650 7 a| Supersonic combustion ramjet engines.2| nasat;

650 7 a| Simulation.2| nasat;

700 1 a| Yungster, Shaye,e| author.=| ^A438742;

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

776 08 i| Microfiche version:a| Steffen, Christopher J.t| Computational analysis of the combustion process in an axisymmetric RBCC flowpathw| (OCoLC)50752542;

830 0 a| NASA technical memorandumv| 2001-210679.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/LPS23048;

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

596 a| 1;

998 a| 4792538;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4792538-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 12/8/2017x| EDOCUMENTz| JERESOURCE;

Computational analysis of the combustion process in an axisymmetric,RBCC flowpath / Christopher J. Steffen, Shaye Yungster.

Author/creator	Steffen, Christopher J. author.
Other author	Yungster, Shaye, author.
Other author	NASA Glenn Research Center, issuing body.
Format	Electronic
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2001.
Description	1 online resource (15 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS23048

Variant title	Computational analysis of the combustion processes in an axisymmetric, rocket based combined cycle flowpath
Series	NASA/TM ; 2001-210679 NASA technical memorandum 2001-210679. ^A467613
General note	"February 2001."
General note	"Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting cosponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000."
General note	"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 15).
Report note	Technical memorandum.
Funding information	Sponsored by the National Aeronautics and Space Administration WU-708-65-13-00 d E-12606
Source of description	Description based on online resource; title from PDF title page (NASA, viewed Nov. 20, 2017).
Issued in other form	Microfiche version: Steffen, Christopher J. Computational analysis of the combustion process in an axisymmetric RBCC flowpath
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:210679

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Computational analysis of the combustion process in an axisymmetric,RBCC flowpath / Christopher J. Steffen, Shaye Yungster.

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