Using the same input design data for the ifr turbine given, Mechanical Engineering

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Using the same input design data for the ifr turbine given

Using the same input design data for the IFR turbine given in Problem 5 and given that the total-to-static efficiency is 0.8, determine

a. the stagnation pressure of the gas at inlet and

b. the total-to-total efficiency of the turbine

Problem 5

The radial-inflow turbine in Problem 3 is designed for a specific speed Ωs of 0.55 rad. Determine

a. the volume flow rate and the turbine power output;

b. the rotor exit hub and tip diameters;

c. the nozzle exit flow angle and the rotor inlet passage width diameter ratio, b2/D2.

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Mechanical Engineering: Using the same input design data for the ifr turbine given

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Mechanical Engineering: Using the same input design data for the ifr turbine given

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