Numerical Investigation of Flow Separation Control on a Highly Loaded Compressor Cascade by Plasma Aerodynamic Actuation-Reference-Cited by-同舟云学术

Numerical Investigation of Flow Separation Control on a Highly Loaded Compressor Cascade by Plasma Aerodynamic Actuation

Published:2012-06 Issue:3 Volume:25 Page:349-360
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

ZHAO Xiaohu,LI Yinghong,WU Yun,ZHU Tao,LI Yiwen

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference21 articles.

1. Merchant A A, Kerrebrock J L. Experimental investigation of a high pressure ratio aspirated fan stage. ASME Paper, GT-2004-53679, 2004.

2. Aerodynamic blade row interactions in an axial compressor: Part I—Unsteady boundary layer development;Mailach;ASME Journal of Turbomachinery,2004

3. Aerodynamic blade row interactions in an axial compressor: Part II—Unsteady profile pressure distrubtion and blade forces;Mailach;ASME Journal of Turbomachinery,2004

4. Analysis of the aerodynamic performance of a super highly loaded adsorption type compressor cascade;Chen;Journal of Engineering for Thermal Energy & Power,2009

5. Lewin E, Kožulovic D, Stark U. Experimental and Numerical analysis of hub-corner stall in compressor cascades. ASME Paper, GT-2010-22704, 2010.

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