LEADER 02201nam  2200589   450 
001 9910702113803321
005 20130115150042.0
035   $a(CKB)5470000002425004
035   $a(OCoLC)824456134
035   $a(EXLCZ)995470000002425004
100   $a20130115d2012      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aImplementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade /$fAli A. Ameri
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (25 pages) $cillustrations
225 1 $a[NASA contractor report] ;$vNASA-CR 2012-217436
300   $aTitle from title screen (viewed Jan. 15, 2013).
300   $a"April 2012."
300   $a"This work was sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center."
320   $aIncludes bibliographical references (pages 24-25).
606   $aComputational fluid dynamics$2nasat
606   $aTurbulent boundary layer$2nasat
606   $aTurbine blades$2nasat
606   $aHeat transfer$2nasat
606   $aLosses$2nasat
606   $aLow Reynolds number$2nasat
606   $aPressure ratio$2nasat
606   $aThree dimensional flow$2nasat
606   $aLaminar flow$2nasat
615  7$aComputational fluid dynamics.
615  7$aTurbulent boundary layer.
615  7$aTurbine blades.
615  7$aHeat transfer.
615  7$aLosses.
615  7$aLow Reynolds number.
615  7$aPressure ratio.
615  7$aThree dimensional flow.
615  7$aLaminar flow.
700   $aAmeri$b Ali A.$01384587
712 02$aNASA Glenn Research Center,
712 02$aFundamental Aeronautics Program (U.S.),
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702113803321
996   $aImplementation of a transition model in a NASA code and validation using heat transfer data on a turbine blade$93511555
997   $aUNINA