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A gas turbine has two stages of ideal compression, expansion, intercooling, and reheating. Air enters the first compressor at 13psia and 60F; the total pressure ratio (across all compressors) is 12; the total rate of heat addition is 500 Btu/s; and the cold air temperature is increased by 50F in the regenerator. Calculate the power produced by each turbine, power consumed by each compressor, and the rate of heat rejection. Use constant specific heats at room temperature.
in many vacuum systems there is a gate valve consisting of a gasketed metal plate that acts to isolate the chamber
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the structural engineering design section within the engineering department of a regional natural gas corporation has
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