Gas Turbine Blade Cooling Technology, Advances, and Challenges

Date

2019-09-30

Author

Kahveci, Harika Senem

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Continuous advances in cooling technologies have become necessary since the engine thermal efficiency and power output increase significantly with an increase in the turbine inlet temperature. This study explains blade cooling techniques and discusses the related challenges and recent advances in this research field.

URI

http://aiac.ae.metu.edu.tr/program/paper.php?No=AIAC-2019-105
https://hdl.handle.net/11511/80936

Conference Name

10th Ankara International Aerospace Conference, Ankara, Türkiye, 18 - 20 Eylül 2019

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

H. S. Kahveci, “Gas Turbine Blade Cooling Technology, Advances, and Challenges,” presented at the 10th Ankara International Aerospace Conference, Ankara, Türkiye, 18 - 20 Eylül 2019, Ankara, Türkiye, 2019, Accessed: 00, 2021. [Online]. Available: http://aiac.ae.metu.edu.tr/program/paper.php?No=AIAC-2019-105.