LEADER 02589nam 2200625Ia 450 001 9910699641303321 005 20110419081447.0 035 $a(CKB)5470000002404524 035 $a(OCoLC)705353528 035 $a(EXLCZ)995470000002404524 100 $a20110304d2010 ua 0 101 0 $aeng 135 $aurmn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aComparing spray characteristics from Reynolds Averaged Navier-Stokes (RANS) National Combustion Code (NCC) calculations against experimental data for a turbulent reacting flow$b[electronic resource] /$fAnthony C. Iannetti and Jeffery P. Moder ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 4-7, 2010 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010] 215 $a1 online resource (v, 39 pages) $cillustrations 225 1 $aNASA/TM ;$v2010-216735 300 $aTitle from title screen (viewed on March 4, 2011). 300 $a"July 2010." 300 $a"AIAA-2010-578." 320 $aIncludes bibliographical references (pages 37-39) 517 $aComparing spray characteristics from Reynolds Averaged Navier-Stokes 606 $aComputational fluid dynamics$2nasat 606 $aTurbulent flow$2nasat 606 $aSpray characteristics$2nasat 606 $aJet engine fuels$2nasat 606 $aReaction kinetics$2nasat 606 $aHydrocarbons$2nasat 606 $aSulfur dioxides$2nasat 606 $aNitrogen oxides$2nasat 606 $aExhaust emission$2nasat 606 $aFuel injection$2nasat 615 7$aComputational fluid dynamics. 615 7$aTurbulent flow. 615 7$aSpray characteristics. 615 7$aJet engine fuels. 615 7$aReaction kinetics. 615 7$aHydrocarbons. 615 7$aSulfur dioxides. 615 7$aNitrogen oxides. 615 7$aExhaust emission. 615 7$aFuel injection. 700 $aIannetti$b Anthony C$01407520 701 $aModer$b Jeffrey P$01395515 712 02$aNASA Glenn Research Center. 712 12$aAIAA Aerospace Sciences Meeting$d(48th :$f2010 :$eOrlando, Fla.) 801 0$bGPO 801 1$bGPO 906 $aBOOK 912 $a9910699641303321 996 $aComparing spray characteristics from Reynolds Averaged Navier-Stokes (RANS) National Combustion Code (NCC) calculations against experimental data for a turbulent reacting flow$93514992 997 $aUNINA