Experimental investigation about the circumferential treating angle of non-axisymmetric casing treatments
|更新时间:2026-07-07
|
Experimental investigation about the circumferential treating angle of non-axisymmetric casing treatments
Vol. 24, Issue 6, (2009)
作者机构:
北京航空航天大学 能源与动力工程学院 航空发动机气动热力重点实验室,北京,100191
作者简介:
基金信息:
DOI:
CLC:
Published:2009
稿件说明:
移动端阅览
LIU Jian-yong, YUAN Wei, LU Ya-jun. Experimental investigation about the circumferential treating angle of non-axisymmetric casing treatments[J]. 2009, 24(6).
DOI:
LIU Jian-yong, YUAN Wei, LU Ya-jun. Experimental investigation about the circumferential treating angle of non-axisymmetric casing treatments[J]. 2009, 24(6).DOI:
Experimental investigation about the circumferential treating angle of non-axisymmetric casing treatments
In order to solve the problem that traditional casing treatment increases the stall margin while reducing the efficiency of compressor
five innovative non-axisymmetric casing treatments with different circumferential treating angles were designed in this paper.In a series of experiments
the stall margin of a compressor increased with the rise of circumferential treating angle
while the isentropic efficiency rose up firstly and fell down later.It was interesting that the stall margin and efficiency of the compressor were both enhanced when the circumferential treating angle of the non-axisymmetric casing treatment was 120°
the reason of which was simply attributable to the fact that non-axisymmetric configuration changed the unsteady tip flow in the compressor.