摘要
针对一亚声速单级轴流压气机试验台,根据正交试验的要求设计了9种周向槽机匣处理结构.以其为载体系统地研究了槽式机匣几何结构参数对其扩稳效果的影响.正交实验结果表明:在两种换算转速下无需对所用可能组合的处理机匣结构进行试验,使用正交分析方法对试验结果进行分析都能成功预测扩稳效果最好的处理机匣结构型式.
Nine kinds of circumferential grooved casing treatment structures were designed by the orthogonal experiment s requirement.Optimized experiments of the geometry structure of circumferential groove were performed on a single stage subsonic axial compressor with the nine kinds of circumferential grooved casing treatment structures at two rotor speeds.The results of orthogonal experiments show that the orthogonal experiments are successful.It is not necessary to test all casing treatment of possible combinatio...
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2009年第4期825-829,共5页
Journal of Aerospace Power
基金
自然科学基金(50506026)
航空基金(2007ZB53021)
航空科技创新基金(08B53004)
西北工业大学基础研究基金(W018101)
关键词
压气机
机匣处理
结构
正交试验
compressor
casing treatment
structure
orthogonal experiment