Study of loss mechanism in low speed compressor cascade using dissipation function
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Study of loss mechanism in low speed compressor cascade using dissipation function
Vol. 26, Issue 2, (2011)
作者机构:
哈尔滨工业大学 能源科学与工程学院 推进理论与技术研究所,哈尔滨,150001
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Published:2011
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LIU Hua-ping, CHEN Huan-long, YANG Xiao-guang, et al. Study of loss mechanism in low speed compressor cascade using dissipation function[J]. 2011, 26(2).
DOI:
LIU Hua-ping, CHEN Huan-long, YANG Xiao-guang, et al. Study of loss mechanism in low speed compressor cascade using dissipation function[J]. 2011, 26(2).DOI:
Study of loss mechanism in low speed compressor cascade using dissipation function
The transport equation of total pressure containing dissipation function was derived.Through experimental and numerical studies of a low speed compressor cascade
the characteristics of flow and loss distribution were discussed in detail
then the loss mechanism was obtained.The results show that:the high cascade loss originates from dissipation in the area near the blade leading edge
blade and end wall surface
wakes
as well as the area between the separation and mainstream.Moreover
the separation zone is only a low-energy fluid gathering area for large total pressure loss and entropy rather than a zone of loss source.The essences of improving the cascade performance by controlling separation are weakening the shear strength and reducing the strong shear zone in the area between the separation and mainstream by increasing the velocity and reducing separation area.A method of improving the cascade performance by controlling the evolution of boundary layer and horseshoe vortex at the cascade inlet is recommended.This paper presents a new thought of controlling cascade losses.