Effects of tip clearance flow on aerodynamic performance of transonic axial compressor rotor
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Effects of tip clearance flow on aerodynamic performance of transonic axial compressor rotor
Thermal Power GenerationVol. 43, Issue 12, Pages: 72-76(2014)
作者机构:
1. 西安热工研究院有限公司
2. 西安交通大学能源与动力工程学院
作者简介:
基金信息:
DOI:
CLC:TH453
Published:2014
稿件说明:
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LI Yuanyuan, ZHANG Chuhua, XIAO Junfeng, et al. Effects of tip clearance flow on aerodynamic performance of transonic axial compressor rotor[J]. Thermal power generation, 2014, 43(12): 72-76.
DOI:
LI Yuanyuan, ZHANG Chuhua, XIAO Junfeng, et al. Effects of tip clearance flow on aerodynamic performance of transonic axial compressor rotor[J]. Thermal power generation, 2014, 43(12): 72-76.DOI:
Effects of tip clearance flow on aerodynamic performance of transonic axial compressor rotor
the internal three-dimensional turbulent flow field of a transonic axial compressor Rotor37 with seven tip clearances is numerically studied.The effects of tip clearance flow on aerodynamic performance of the transonic axial compressor rotor are investigated.The results show that
with a decrease in the tip clearance
the aerodynamic efficiency and pressure ratio increase and the stable operation area enlarges significantly.The relationship between the aerodynamic performance and the tip clearance deviates far away from the linear function and appears the curve characteristics.For this rotor
the optimal tip clearance 0.178 mm is a compromise between aerodynamic and structural requirements.