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001 9910706184803321
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035   $a(EXLCZ)995470000002454576
100   $a20170821j199901    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPrediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn /$fDavid L. Rigby
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dJanuary 1999.
215   $a1 online resource (12 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-208501
300   $a"January 1999."
300   $a"Prepared for the 43rd Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Stockholm, Sweden, June 2-5, 1998."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 11-12).
606   $aReynolds averaging$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aNavier-Stokes equation$2nasat
606   $aTurbine blades$2nasat
606   $aCooling systems$2nasat
606   $aMass transfer$2nasat
606   $aHeat transfer$2nasat
606   $aK-omega turbulence model$2nasat
606   $aEngine coolants$2nasat
606   $aComputational grids$2nasat
615  7$aReynolds averaging.
615  7$aComputational fluid dynamics.
615  7$aNavier-Stokes equation.
615  7$aTurbine blades.
615  7$aCooling systems.
615  7$aMass transfer.
615  7$aHeat transfer.
615  7$aK-omega turbulence model.
615  7$aEngine coolants.
615  7$aComputational grids.
700   $aRigby$b D. L$g(David Lester),$f1963-$01414359
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706184803321
996   $aPrediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn$93546179
997   $aUNINA