LEADER 01994nam  2200505I  450 
001 9910703786003321
005 20150807160136.0
035   $a(CKB)5470000002433858
035   $a(OCoLC)916511610
035   $a(EXLCZ)995470000002433858
100   $a20150807j201411    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComputational investigation of novel tip leakage mitigation methods for high pressure turbine blades /$fMounir Ibrahim and Abhinav Gupta, Vikram Shyam
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dNovember 2014.
215   $a1 online resource (19 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2014-218494
300   $aTitle from title screen (viewed Aug. 7, 2015).
300   $a"November 2014."
300   $a"Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014."
320   $aIncludes bibliographical references (page 19).
606   $aComputational fluid dynamics$2nasat
606   $aTurbine blades$2nasat
606   $aRotor blades (turbomachinery)$2nasat
606   $aHole distribution (mechanics)$2nasat
606   $aHole geometry (mechanics)$2nasat
615  7$aComputational fluid dynamics.
615  7$aTurbine blades.
615  7$aRotor blades (turbomachinery)
615  7$aHole distribution (mechanics)
615  7$aHole geometry (mechanics)
700   $aIbrahim$b Mounir B.$0477244
702   $aGupta$b Abhinav
702   $aShyam$b Vikram
712 02$aNASA Glenn Research Center,
712 02$aFundamental Aeronautics Program (U.S.),
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703786003321
996   $aComputational investigation of novel tip leakage mitigation methods for high pressure turbine blades$93521640
997   $aUNINA