Engineering
Engineering, 19.02.2020 04:02, gunaranjan09

Air flows through an air turbine where its stagnation pressure is decreased in the ratio 5:1. The total-to-total efficiency is 0.8 and the air flow rate is 5 kg/s. If the total power output is 500 kW, find (a) inlet total temperature. (b) the actual exit total temperature. (c) the actual exit static temperature if the flow velocity is 100 m/s. (d) the total-to-static efficiency of the device.

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