LEADER 02059nam  2200517   450 
001 9910707309003321
005 20160803115058.0
035   $a(CKB)5470000002464432
035   $a(OCoLC)954593999
035   $a(EXLCZ)995470000002464432
100   $a20160803j199611    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPredicted turbine heat transfer for a range of test conditions /$fR.J. Boyle and B.L. Lucci
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dNovember 1996.
215   $a1 online resource (16 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107374
300   $aTitle from title screen (viewed Aug. 3, 2016).
300   $a"November 1996"--Report documentation page.
300   $a"Prepared for the 41st Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Birmingham, United Kingdom, June 10-13, 1996."
300   $a"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 16).
606   $aAerodynamic characteristics$2nasat
606   $aHeat transfer$2nasat
606   $aTurbulence models$2nasat
606   $aTurbine blades$2nasat
606   $aWall flow$2nasat
606   $aNavier-Stokes equation$2nasat
615  7$aAerodynamic characteristics.
615  7$aHeat transfer.
615  7$aTurbulence models.
615  7$aTurbine blades.
615  7$aWall flow.
615  7$aNavier-Stokes equation.
700   $aBoyle$b Robert J.$01387461
702   $aLucci$b Barbara L.
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707309003321
996   $aPredicted turbine heat transfer for a range of test conditions$93437387
997   $aUNINA