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초소형 원심압축기의 날개 두께 변화에 따른 성능에 관한 실험적 연구
강신형,조운제,윤하용,이승갑,Kang, Shin-Hyoung,Cho, Woon-Je,Yun, Ha-Yong,Lee, Seung-Kap 한국유체기계학회 1999 한국유체기계학회 논문집 Vol.2 No.1
Some sized centrifugal compressors were designed and their performance measured to investigate the effects of exit blade thickness, width and back swept angle. The impeller of larger blade thickness shows low pressure ratio compared with that of smaller ones. Backswept angle also have a large effect on the efficiency. Measured values of slip factor are quite different from the estimated values of the Wiesner-Busemann model and an increase in the flow late.
초소형 원심압축기의 날개 두께 변화에 따른 성능에 관한 실험적 연구
강신형(Shin-Hyoung Kang),조운제(Woon-Je Cho),윤하용(Hayong Yun),이승갑(SeungKap Lee) 한국유체기계학회 1998 유체기계 연구개발 발표회 논문집 Vol.- No.-
Some sized centrifugal compressor were designed and their performance measured to investigate the effects of exit blade thickness, width and back swept angle. The impeller of larger blade thickness shows low pressure ratio compared with that of smaller one. Backswept angle have also large effect on the efficiency. Measured values of slip factor are quite different from the estimated values of Wiesner-Busemann model and increase with the flow rate.