IGTC-3 Experimental Investigation of a Backswept Centrifugal Compressor Impeller(Session A-1 AERODYNAMICS I (Radial Flow))

スポンサーリンク

概要

• 論文の詳細を見る

• Tests of a centrifugal compressor impeller with 25 deg of backswept operating in 250 to 380 m/s tip speed were conducted. Compared with a radial discharge impeller, stage efficiency has increased 4 points, and flow range expended by 17 percent. This paper discribes the flow characteristics of fluid in impeller, and the effect of impeller structure on compressor performance. The data of slip factor and work factor deduced from tests can be applied to compressor performance prediction.

• 社団法人日本ガスタービン学会の論文

著者

• Diao Z.-g.

  Institute Of Engineering Thermophysics Academia Sinica

• Chen J.-Y.

  Institute of Engineering Thermophysics, Academia Sinica

• Cao X.-J.

  Institute of Engineering Thermophysics, Academia Sinica

• Cao X.-j.

  Institute Of Engineering Thermophysics Academia Sinica

• Chen J.-y.

  Institute Of Engineering Thermophysics Academia Sinica

関連論文

• IGTC-3 Experimental Investigation of a Backswept Centrifugal Compressor Impeller(Session A-1 AERODYNAMICS I (Radial Flow))

スポンサーリンク