Flow Field Improvement by Bowed Stator Stages in a Compressor with Different Axial Gaps Under Near Stall Condition-Reference-Cited by-同舟云学术

Flow Field Improvement by Bowed Stator Stages in a Compressor with Different Axial Gaps Under Near Stall Condition

Published:2008-06 Issue:3 Volume:21 Page:215-222
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

Huawei Lu,Fu Chen,Jilin Wan,Zhongqi Wang

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference16 articles.

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2. Breugelmans F A E. Influence of incidence angle on the secondary flow in compressor cascade with different dihedral distribution. ISABE 85-7078, 1985.

3. Comparison of sweep and dihedral effects on compressor cascade performance;Sasaki;Journal of Turbomachinery,1998

4. Direct and inverted calculation of 2D axisymmetric and 3D flows in axial compressor blade rows;Bogod;Revue Francaise de Mecanique,1992

5. Li S B. Design of highly loaded dihedral stator and investigation on the aerodynamic stage performance in an axial transonic compressor. PhD thesis, Harbin Institute of Technology, 2007. [in Chinese].

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