Engineering, 09.02.2022 14:00 triddi666
In a gas-turbine cycle, fuel is combusted with air in a constant-pressure combustion chamber at a pressure of 0.8 MPa. The combustion process can simplified by (1) assuming that it could be represented as a heat-addition process and (2) neglecting the mass flowrate of the fuel (i. e. assuming that only air goes in and out of the combustion chamber).
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In a gas-turbine cycle, fuel is combusted with air in a constant-pressure combustion chamber at a pr...
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