![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)
Applied Sciences | Free Full-Text | Comparison of Cooling Different Parts in a High Pressure Ratio Centrifugal Compressor
![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
![Compressor pressure ratio and efficiency lines as a function of mass... | Download Scientific Diagram Compressor pressure ratio and efficiency lines as a function of mass... | Download Scientific Diagram](https://www.researchgate.net/publication/245353081/figure/fig3/AS:385265102278658@1468865766710/Compressor-pressure-ratio-and-efficiency-lines-as-a-function-of-mass-flow-and-rotational.png)
Compressor pressure ratio and efficiency lines as a function of mass... | Download Scientific Diagram
![fuel - Why a higher compressor pressure ratio results in higher Thrust and lower TSFC? - Aviation Stack Exchange fuel - Why a higher compressor pressure ratio results in higher Thrust and lower TSFC? - Aviation Stack Exchange](https://i.stack.imgur.com/35rLz.png)
fuel - Why a higher compressor pressure ratio results in higher Thrust and lower TSFC? - Aviation Stack Exchange
![Effects of Compressor Pressure Ratio and Combustion Chamber Exhaust Gases Temperatures on Gas Turbine Cycle Performance | Semantic Scholar Effects of Compressor Pressure Ratio and Combustion Chamber Exhaust Gases Temperatures on Gas Turbine Cycle Performance | Semantic Scholar](https://d3i71xaburhd42.cloudfront.net/332872fd9bb0bc59a49ec37a192e5ce31695f71d/4-Figure4-1.png)