![Applied Sciences | Free Full-Text | Heat Transfer Analysis in a Single Spool Gas Turbine by Using Calculated-Estimated Coefficients with the Finite Element Method Applied Sciences | Free Full-Text | Heat Transfer Analysis in a Single Spool Gas Turbine by Using Calculated-Estimated Coefficients with the Finite Element Method](https://www.mdpi.com/applsci/applsci-10-08328/article_deploy/html/images/applsci-10-08328-g001.png)
Applied Sciences | Free Full-Text | Heat Transfer Analysis in a Single Spool Gas Turbine by Using Calculated-Estimated Coefficients with the Finite Element Method
![Effect of ambient temperature on the CCGT heat rate and steam mass flow... | Download Scientific Diagram Effect of ambient temperature on the CCGT heat rate and steam mass flow... | Download Scientific Diagram](https://www.researchgate.net/publication/233532746/figure/fig7/AS:300016276131843@1448540862232/Effect-of-ambient-temperature-on-the-CCGT-heat-rate-and-steam-mass-flow-rate.png)
Effect of ambient temperature on the CCGT heat rate and steam mass flow... | Download Scientific Diagram
![Mass flow rate and temperature exhaust from GE10 gas turbine, varying... | Download Scientific Diagram Mass flow rate and temperature exhaust from GE10 gas turbine, varying... | Download Scientific Diagram](https://www.researchgate.net/publication/339667119/figure/fig1/AS:865166560346112@1583283190390/Mass-flow-rate-and-temperature-exhaust-from-GE10-gas-turbine-varying-ambient-temperature.png)
Mass flow rate and temperature exhaust from GE10 gas turbine, varying... | Download Scientific Diagram
![Combustion gases enter a gas turbine at 627 ^{\circ}C and 1.2 MPa at a rate of 2.5 kg/s and leave at 527 ^{\circ}C and 500 kPa. It is estimated that heat is Combustion gases enter a gas turbine at 627 ^{\circ}C and 1.2 MPa at a rate of 2.5 kg/s and leave at 527 ^{\circ}C and 500 kPa. It is estimated that heat is](https://homework.study.com/cimages/multimages/16/capture_3623994150029290475296.jpg)
Combustion gases enter a gas turbine at 627 ^{\circ}C and 1.2 MPa at a rate of 2.5 kg/s and leave at 527 ^{\circ}C and 500 kPa. It is estimated that heat is
![Effect of inlet ambient temperature on the gas turbine performance ( =... | Download Scientific Diagram Effect of inlet ambient temperature on the gas turbine performance ( =... | Download Scientific Diagram](https://www.researchgate.net/publication/312625572/figure/fig2/AS:613508890767397@1523283326540/Effect-of-inlet-ambient-temperature-on-the-gas-turbine-performance-0006284.png)