Problem 6. (8 points) Air with density of 1.38 kg/m3 enters a reaction axial-flow turbine at 172 m/s in the direction of
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Problem 6. (8 points) Air with density of 1.38 kg/m3 enters a reaction axial-flow turbine at 172 m/s in the direction of
Problem 6. (8 points) Air with density of 1.38 kg/m3 enters a reaction axial-flow turbine at 172 m/s in the direction of 62% with respect to the axis. If the rotor has dimensions n=0.34 m and n = 0.20 m and is rotating at 4800 rpm, determine the blade angles at the mean radii of both the inlet and outlet and estimate its output shaft power. Tan = [ (1? +n?)/2]'? A = 1 (1-1). P. = maur U (V1 + V.2). D