A gas turbine for an automobile is designed with a regenerator. Air enters the compressor of this engine at 100 kPa and 30°C. The compressor pressure ratio is 8, the maximum cycle temperature is 800°C, and the cold airstream leaves the regenerator 10°C cooler than the hot airstream at the inlet of the regenerator. Assuming both the compressor and the turbine to be isentropic, determine the rates of heat addition and rejection for this cycle when it produces 105 kW. Use constant specific heats at room temperature. The properties of air at room temperature are cp=1.005 kJ/kg-K and k=1.4. Compressor Heat exchanger Comb Turbine The rate of heat addition for this cycle is The rate of heat rejection for this cycle is KW. kW.
A gas turbine for an automobile is designed with a regenerator. Air enters the compressor of this engine at 100 kPa and 30°C. The compressor pressure ratio is 8, the maximum cycle temperature is 800°C, and the cold airstream leaves the regenerator 10°C cooler than the hot airstream at the inlet of the regenerator. Assuming both the compressor and the turbine to be isentropic, determine the rates of heat addition and rejection for this cycle when it produces 105 kW. Use constant specific heats at room temperature. The properties of air at room temperature are cp=1.005 kJ/kg-K and k=1.4. Compressor Heat exchanger Comb Turbine The rate of heat addition for this cycle is The rate of heat rejection for this cycle is KW. kW.
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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