Computation of flow through transonic axial compressor cascade, for the blade with non-linear load and non-linear tangent velocity radial design, by using the active disk theory

被引：0

作者：

Andrei, Irina Carmen ^{[1
]}

Berbente, C. ^{[1
]}

Berbente, S. ^{[1
]}

机构：

[1] Univ Politehn Bucuresti, Fac Aerosp Engn, Bucharest 011061, Romania

来源：

FMA'08: PROCEEDINGS OF THE 6TH IASME/WSEAS INTERNATIONAL CONFERENCE ON FLUID MECHANICS AND AERODYNAMICS: NEW ASPECTS OF FLUID MECHANICS AND AERODYNAMICS | 2008年

关键词：

axial flow compressor; cascade; active disk theory; aerodynamics; computation; blade's radial design;

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper presents a study regarding the application of the active disk theory ADT to a transonic rotor with transonic rotor, featuring non-linear spanwise distribution of the blade loading and non-linear tangent velocity radial design, in purpose to calculating the velocities within the computation domain. A comparison between the reference case Marble, [35] and the test case was presented. On account of the obtained results, it was shown that the application of ADT can be extended to far more complex study cases.

引用

页码：287 / 292

页数：6