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1. The adiabatic compressor of a large gas turbine receives air from the ambient surroundings at 95 kPa and 20°C with a low (negligible) velocity. At the compressor discharge, air exits at 1.52 MPa and 430°C with velocity of 90 m/s. The power input to the compressor is 5000 kW. Determine the mass flow rate of air through the unit.
2. Air enters a compressor at 100 kPa and 300 K and is compressed to 150 kPa. The efficiency is 70%. What is the required work input per kg of air? What is the exit temperature?
product and engineering design review8 x product engineering and design review week 2 ndash 12 3 pages per item which
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