Numerical analysis and design optimization on full coverage film-cooling for turbine guided vane
Based on numerical simulations, the heat transfer and flow field of a turbine vane are analyzed and the film cooling is improved. The optimization objective is increasing the overall cooling effectiveness with cascade pressure loss factors staying almost unchanged. Thus, cylindrical film holes were...
Main Authors: | Mingrui Wang, Huiren Zhu, Cunliang Liu, Tao Guo, Li Zhang, Na Li |
---|---|
Format: | Article |
Language: | English |
Published: |
Taylor & Francis Group
2022-12-01
|
Series: | Engineering Applications of Computational Fluid Mechanics |
Subjects: | |
Online Access: | https://www.tandfonline.com/doi/10.1080/19942060.2021.2019127 |
Similar Items
-
The film cooling performance of spiral-channel holes on turbine guide vane
by: Yuhao Jia, et al.
Published: (2024-01-01) -
Flat Plate and Turbine Vane Film-Cooling Performance with Laid-Back Fan-Shaped Holes
by: Tommaso Bacci, et al.
Published: (2019-06-01) -
Experimental Optimization of the Compound Angled Asymmetric Laidback Fan Shaped Film Cooling Hole
by: Ye Rim Jo, et al.
Published: (2022-10-01) -
Effects of Gas Thermophysical Properties on the Full-Range Endwall Film Cooling of a Turbine Vane
by: Jian Liu, et al.
Published: (2023-06-01) -
Conjugate Heat Transfer Simulation of Overall Cooling Performance for Cratered Film Cooling Holes
by: Chao Zhang, et al.
Published: (2022-05-01)