کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
757654 | 1462551 | 2008 | 7 صفحه PDF | دانلود رایگان |
![عکس صفحه اول مقاله: Aerodynamic Design and Analysis of a Low-reaction Axial Compressor Stage Aerodynamic Design and Analysis of a Low-reaction Axial Compressor Stage](/preview/png/757654.png)
There is introduced a new low-reaction, highly-loaded axial compressor design concept which is coupled with boundary layer suction method. The characteristic features of the concept are made clear through its comparison with the MIT boundary layer suction compressor. Also are pointed out the potential applications of this concept as well as its key technological problems. Based on this concept, a single-stage, low-reaction and low-speed axial compressor is constructed in association with analysis and computation of boundary layer suction on vanes with the aid of a three-dimensional numerical approach. The results attest to the effectiveness of this way to control separation in blade cascades by the boundary layer suction and the feasibility of this proposed design concept.
Journal: Chinese Journal of Aeronautics - Volume 21, Issue 1, February 2008, Pages 1-7