LEADER 01930nam  2200517   450 
001 9910705859603321
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035   $a(CKB)5470000002453820
035   $a(OCoLC)995164631
035   $a(EXLCZ)995470000002453820
100   $a20170727j199806    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMach number effects on turbine blade transition length prediction /$fR.J. Boyle and F.F. Simon
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$dJune 1998.
215   $a1 online resource (12 pages) $cillustrations
225 1 $aNASA/TM ;$v1998-208404
300   $a"June 1998."
300   $a"Prepared for the Turbo Expo '98 sponsored by 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.
300   $a"98-GT-367."
320   $aIncludes bibliographical references (pages 11-12).
606   $aMach number$2nasat
606   $aTurbine blades$2nasat
606   $aMathematical models$2nasat
606   $aTurbulence models$2nasat
606   $aNavier-Stokes equation$2nasat
606   $aBoundary layer transition$2nasat
615  7$aMach number.
615  7$aTurbine blades.
615  7$aMathematical models.
615  7$aTurbulence models.
615  7$aNavier-Stokes equation.
615  7$aBoundary layer transition.
700   $aBoyle$b Robert J.$01387461
702   $aSimon$b F. F$g(Frederick F.),
712 02$aLewis Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705859603321
996   $aMach number effects on turbine blade transition length prediction$93473392
997   $aUNINA