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Effects of Compressor Pressure Ratio and Combustion Chamber Exhaust Gases Temperatures on Gas Turbine Cycle Performance | Semantic Scholar
![Air enters the compressor of a simple gas turbine at 0.1 MPa, 300 K. The pressure ratio is 16 and the maximum temperature is 1000 K. The turbine process is divided into Air enters the compressor of a simple gas turbine at 0.1 MPa, 300 K. The pressure ratio is 16 and the maximum temperature is 1000 K. The turbine process is divided into](https://homework.study.com/cimages/multimages/16/fig173630432432069200931.png)
Air enters the compressor of a simple gas turbine at 0.1 MPa, 300 K. The pressure ratio is 16 and the maximum temperature is 1000 K. The turbine process is divided into
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Applied Sciences | Free Full-Text | Comparison of Cooling Different Parts in a High Pressure Ratio Centrifugal Compressor
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