LEADER 02299nam  2200517   450 
001 9910706576003321
005 20171120092821.0
035   $a(CKB)5470000002456685
035   $a(OCoLC)1012398455
035   $a(EXLCZ)995470000002456685
100   $a20171120j200102    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComputational analysis of the combustion process in an axisymmetric,RBCC flowpath /$fChristopher J. Steffen, Shaye Yungster
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dFebruary 2001.
215   $a1 online resource (15 pages) $cillustrations
225 1 $aNASA/TM ;$v2001-210679
300   $a"February 2001."
300   $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."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
320   $aIncludes bibliographical references (page 15).
517 3 $aComputational analysis of the combustion processes in an axisymmetric, rocket based combined cycle flowpath
606   $aComputational fluid dynamics$2nasat
606   $aNumerical analysis$2nasat
606   $aCombustion physics$2nasat
606   $aThree dimensional models$2nasat
606   $aSupersonic combustion ramjet engines$2nasat
606   $aSimulation$2nasat
615  7$aComputational fluid dynamics.
615  7$aNumerical analysis.
615  7$aCombustion physics.
615  7$aThree dimensional models.
615  7$aSupersonic combustion ramjet engines.
615  7$aSimulation.
700   $aSteffen$b Christopher J.$01386995
702   $aYungster$b Shaye
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706576003321
996   $aComputational analysis of the combustion process in an axisymmetric,RBCC flowpath$93436394
997   $aUNINA