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作 者:孙晓峰[1] 胡宗安[1] 冯毓诚[1] 周盛[1]
机构地区:[1]北京航空航天大学
出 处:《航空动力学报》1991年第2期129-130,共2页Journal of Aerospace Power
摘 要:According to analysis of the characteristics of frequency and propagation of the sound generated by the rotating stall,an acoustic measuring method is developed,in which the characteristic parameters,such as the number and propagation speed of stall cells,are measured.Compared with existing methods,this method is a untouched measurement so as to avoid not disturb ance of the flow field .The primary experimental results obtained on a transonic axial-flow compressor facility demostrate the feasibility of this method.According to analysis of the characteristics of frequency and propagation of the sound generated by the rotating stall,an acoustic measuring method is developed,in which the characteristic parameters,such as the number and propagation speed of stall cells,are measured.Compared with existing methods,this method is a untouched measurement so as to avoid not disturb ance of the flow field .The primary experimental results obtained on a transonic axial-flow compressor facility demostrate the feasibility of this method.
分 类 号:V263.452[航空宇航科学与技术—航空宇航制造工程]
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