01994nam 2200505I 450 991070378600332120150807160136.0(CKB)5470000002433858(OCoLC)916511610(EXLCZ)99547000000243385820150807j201411 ua 0engurcn|||||||||txtrdacontentcrdamediacrrdacarrierComputational investigation of novel tip leakage mitigation methods for high pressure turbine blades /Mounir Ibrahim and Abhinav Gupta, Vikram ShyamCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,November 2014.1 online resource (19 pages) color illustrationsNASA/TM ;2014-218494Title from title screen (viewed Aug. 7, 2015)."November 2014.""Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014."Includes bibliographical references (page 19).Computational fluid dynamicsnasatTurbine bladesnasatRotor blades (turbomachinery)nasatHole distribution (mechanics)nasatHole geometry (mechanics)nasatComputational fluid dynamics.Turbine blades.Rotor blades (turbomachinery)Hole distribution (mechanics)Hole geometry (mechanics)Ibrahim Mounir B.477244Gupta AbhinavShyam VikramNASA Glenn Research Center,Fundamental Aeronautics Program (U.S.),GPOGPOBOOK9910703786003321Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades3521640UNINA