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Compressor pressure ratio and efficiency lines as a function of mass... | Download Scientific Diagram
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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
![Investigate the effects of varying compressor pressure ratio and turbine inlet temperature. Air enters the compressor of an ideal cold-air standard Brayton cycle at 100 kPa, 300 K with a mass flow Investigate the effects of varying compressor pressure ratio and turbine inlet temperature. Air enters the compressor of an ideal cold-air standard Brayton cycle at 100 kPa, 300 K with a mass flow](https://homework.study.com/cimages/multimages/16/t_s_dia8344181553097198041.jpg)
Investigate the effects of varying compressor pressure ratio and turbine inlet temperature. Air enters the compressor of an ideal cold-air standard Brayton cycle at 100 kPa, 300 K with a mass flow
![Applied Sciences | Free Full-Text | Comparison of Cooling Different Parts in a High Pressure Ratio Centrifugal Compressor Applied Sciences | Free Full-Text | Comparison of Cooling Different Parts in a High Pressure Ratio Centrifugal Compressor](https://www.mdpi.com/applsci/applsci-07-00016/article_deploy/html/images/applsci-07-00016-g001.png)