Laser Anemometer Measurements and Computations for Transonic Flow Conditions in an Annular Cascade of High Turning Core Turbine Vanes
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50-percent axial chord 50-percent span aerosol Annular Cascade axial and tangential axial chord fig Axial Radial Tangential axial Solid symbols Axial Standard Circumferential bellmouth boundary layer chord and 50-percent Circumferential position Circumferential Standard Turbulence Comparing the transonic critical velocity ratio denote axial Solid denote tangential Denton's Denton's component calculation design flow results downstream exit critical velocity flow results showed HIGH TURNING CORE hub endwall laser anemometer measurements Laser component measurement mean radius midspan NASA OlVa optical table percent percent deg power law probe volume radial survey Radial Tangential Axial seed particles shown in figure Standard Circumferential Standard Standard Turbulence position symbols denote axial symbols denote tangential TABLE III.-Continued Tangential Axial Standard tangential component tangential Denton's component tangential velocity component transonic and design transonic flow conditions turbine stator vanes TURNING CORE TURBINE vane leading edge vane passage vane suction surface vane trailing edge velocity component difference velocity deviation wakes turbulence