Pipe Diffuser for Radial and Axial-centrifugal Compressor

被引：3
|
作者：
Antas, Stanislaw [1 ]
机构：
[1] Rzeszow Univ Technol, Dept Aircraft & Aircraft Engines, Fac Mech Engn & Aeronaut, Rzeszow, Poland
来源：
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES | 2014年 / 31卷 / 01期
关键词：
turbine engine; compressor; pipe diffuser;
D O I：
10.1515/tjj-2013-0031
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
This paper presents an original method for calculation of geometric parameters of the pipe diffuser and the proposition of a method for determination of flow parameters at the outlet of the diffuser. Proposed methods may be applied for calculations at compressor conceptual design stage. Results of few experimental tests of the pipe diffuser are also presented.
引用
收藏
页码：29 / 36
页数：8
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