LEADER 01944nam  2200529I  450 
001 9910695071803321
005 20170912111821.0
035   $a(CKB)5470000002366000
035   $a(OCoLC)1003322880
035   $a(EXLCZ)995470000002366000
100   $a20170912j199111    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effects of Reynolds number, rotor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage /$freported by M.F. Blair
210  1$aEast Hartford, Connecticut :$cUnited Technologies Research Center,$dNovember 1991.
215   $a1 online resource (vi, 67 pages, 172 unnumbered pages) $cillustrations
225 1 $aNASA CR ;$v184260
300   $a"November 1991."
300   $aDescription based on online resource; title from PDF title page (NASA, viewed Sep. 12, 2017).
320   $aIncludes bibliographical references (pages 53-57).
606   $aAerodynamics$2nasat
606   $aGas turbines$2nasat
606   $aHeat transfer$2nasat
606   $aRotors$2nasat
606   $aThree dimensional flow$2nasat
606   $aTurbine pumps$2nasat
606   $aTurbulence models$2nasat
606   $aViscous flow$2nasat
615  7$aAerodynamics.
615  7$aGas turbines.
615  7$aHeat transfer.
615  7$aRotors.
615  7$aThree dimensional flow.
615  7$aTurbine pumps.
615  7$aTurbulence models.
615  7$aViscous flow.
700   $aBlair$b M. F.$01391724
712 02$aUnited Technologies Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910695071803321
996   $aThe effects of Reynolds number, rotor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage$93486471
997   $aUNINA