Energy- and aerodynamic examination of slightly backward leaning impeller blading of small centrifugal compressors

被引：0

作者：

Pásztor, Endre ^{[1
]}

Varga, Béla ^{[2
]}

机构：

[1] Department of Aeronautics, Naval Architecture and Railway Vehicles, Faculty of Transportation Engineering and Vehicle Engineering, Budapest University of Technology and Economics, Hungary

[2] Department of Military Aviation, National University of Public Service, Ludovika square 2., Budapest,H-1083, Hungary

来源：

Periodica Polytechnica Transportation Engineering | 2015年 / 43卷 / 04期

关键词：

Aerodynamics; -; Impellers; Centrifugation;

D O I：

10.3311/PPtr.8093

中图分类号：

学科分类号：

摘要：

引用

页码：199 / 205

共 4 条

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[3] AERODYNAMIC TESTS ON CENTRIFUGAL PROCESS COMPRESSORS - INFLUENCE OF DIFFUSER DIAMETER RATIO, AXIAL STAGE PITCH, AND IMPELLER CUT BACK
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[4] Effect of impeller structure on aerodynamic performance and noise reduction of a small multi-blade centrifugal fan
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