LEADER 02157nam 2200577I 450 001 9910704876803321 005 20140212130047.0 035 $a(CKB)5470000002444965 035 $a(OCoLC)870179343 035 $a(EXLCZ)995470000002444965 100 $a20140207d2013 ua 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aValidation of a CFD methodology for variable speed power turbine relevant conditions /$fAli A. Ameri, Paul W. Giel, Ashlie B. McVetta 210 1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2013. 215 $a1 online resource (10 pages) $ccolor illustrations 225 1 $aNASA/TM ;$v2013-217860 300 $aTitle from title screen (viewed on Feb. 7, 2014). 300 $a"May 2013." 300 $a"Prepared for the Turbo Expo 2013 sponsored by the American Society of Mechanical Engineers (ASME), San Antonio, Texas, June 3-7, 2013." 300 $a"GT2013-95030." 320 $aIncludes bibliographical references (pages 9-10). 606 $aTurbulence models$2nasat 606 $aThree dimensional flow$2nasat 606 $aComputational fluid dynamics$2nasat 606 $aAerodynamic characteristics$2nasat 606 $aLow Reynolds number$2nasat 606 $aPressure distribution$2nasat 606 $aTransition flow$2nasat 615 7$aTurbulence models. 615 7$aThree dimensional flow. 615 7$aComputational fluid dynamics. 615 7$aAerodynamic characteristics. 615 7$aLow Reynolds number. 615 7$aPressure distribution. 615 7$aTransition flow. 700 $aAmeri$b Ali A.$01384587 702 $aGiel$b P. W$g(Paul W.), 702 $aMcVetta$b Ashlie B. 712 02$aFundamental Aeronautics Program (U.S.), 712 02$aNASA Glenn Research Center, 801 0$bGPO 801 1$bGPO 801 2$bGPO 906 $aBOOK 912 $a9910704876803321 996 $aValidation of a CFD methodology for variable speed power turbine relevant conditions$93541136 997 $aUNINA