02167nam 2200577Ia 450 991070221650332120121203142845.0(CKB)5470000002425987(OCoLC)820022602(EXLCZ)99547000000242598720121203d2012 ua 0engurmn|||||||||txtrdacontentcrdamediacrrdacarrierComparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating[electronic resource] /Vikram Shyam, Ali AmeriCleveland, Ohio :National Aeronautics and Space Administration, Glenn Research Center,[2012]1 online resource (8 pages) illustrations (some color)NASA/TM ;2012-217607Title from title screen (viewed on Dec. 3, 2012)."July 2012.""Prepared for the TURBO EXPO 2011 sponsored by the American Society of Mechanical Engineers (ASME) Vancouver, British Columbia, June 6-10, 2011.""GT2011-46390."Includes bibliographical references (page 8).Computational fluid dynamicsnasatSupersonic turbinesnasatBlade tipsnasatSupersonic flownasatRotor aerodynamicsnasatAxial flow turbinesnasatSupersonic heat transfernasatContoursnasatComputational fluid dynamics.Supersonic turbines.Blade tips.Supersonic flow.Rotor aerodynamics.Axial flow turbines.Supersonic heat transfer.Contours.Shyam Vikram1390439Ameri Ali1406732NASA Glenn Research Center.ASME Turbo Expo(2011 :Vancouver, B.C.)GPOGPOBOOK9910702216503321Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating3486384UNINA