Experimental investigation of the bending clearance on the aerodynamic performance in turbine blade tip region
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DOI: 10.1016/j.energy.2020.117234
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References listed on IDEAS
- Zou, Zhengping & Shao, Fei & Li, Yiran & Zhang, Weihao & Berglund, Albin, 2017. "Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance," Energy, Elsevier, vol. 138(C), pages 167-184.
- Gao, Jie & Zheng, Qun & Xu, Tianbang & Dong, Ping, 2015. "Inlet conditions effect on tip leakage vortex breakdown in unshrouded axial turbines," Energy, Elsevier, vol. 91(C), pages 255-263.
- Cho, Soo-Yong & Cho, Chong-Hyun & Choi, Sang-Kyu, 2017. "An experimental study of partial admission losses with various blade tip clearances using a linear cascade," Energy, Elsevier, vol. 122(C), pages 627-637.
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Cited by:
- Wang, Like & Feng, Jianjun & Lu, Jinling & Zhu, Guojun & Wang, Wei, 2024. "Novel bionic wave-shaped tip clearance toward improving hydrofoil energy performance and suppressing tip leakage vortex," Energy, Elsevier, vol. 290(C).
- Nakhchi, M.E. & Naung, S. Win & Rahmati, M., 2022. "Influence of blade vibrations on aerodynamic performance of axial compressor in gas turbine: Direct numerical simulation," Energy, Elsevier, vol. 242(C).
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Keywords
Bending clearance design; Tip leakage flow; Deformation coefficient; Blocking vortex; Experiment;All these keywords.
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