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An axial-flow turbine stage is to be designed for free-vortex conditions at exit from the nozzle row and for zero swirl at exit from the rotor. The gas entering the stage has a stagnation temperature of 1000 K, the mass flow rate is 32 kg/s, the root and tip diameters are 0.56 m and 0.76 m, respectively, and the rotor speed is 8000 rev/min. At the rotor tip, the stage reaction is 50% and the axial velocity is constant at 183 m/s. The velocity of the gas entering the stage is equal to that leaving. Determine
a. the maximum velocity leaving the nozzles;
b. the maximum absolute Mach number in the stage;
c. the root section reaction;
d. the power output of the stage;
e. the stagnation and static temperatures at stage exit
at room temperature 23oc a cylinder of steel has a diameter of 15.02 mm which is too large to fit into a 15 mm diameter
If the tube surface temperature at the exit is Ts,o 160°C, determine the heat rate entering the tube. Evaluate properties at T 400 K.
Using the tables for water, determine the specific entropy at the indicated states, in Btu/lb ? 8R In each case, locate the state by hand on a sketch of the T-s diagram.
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A hydraulic lift is to be used to lift a 2500 kg weight by putting a weight of 25 kg on a piston with a diameter of 10 cm. Determine the diameter of the piston on which the weight is to be placed.
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