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air-cooled turbine vane airfoil analysis of reference ature blades and vanes computation coolant flow rate coolant inlet pressure Cooling air cooling slot location critical location Critical node CYCLIC STRESS ANALYSIS cyclic tests deceleration failure locations Fatigue cracks fifth cycle film cooling slot flow ratio gas and coolant gas pressure level Gas temperature range gas-flow ratio Gauntner heat transfer analysis high coolant flow high temperature Hot spot Increasing the coolant initiation was predicted inside surface Leading edge crack Lewis Research Center low coolant temperature midchord midspan NASA NASA TN number of cycles operating conditions pressure-surface film cooling psia rapid metal temperature research turbojet engine research vanes sec Figure side film cooling solenoid solenoid valve split trailing edge stagnation point static cascade strain cycles stress analysis program stress concentration stress-strain history suction side film surface film cooling test vanes thermocouples tion transient metal temperatures Vane temperature response Weeton