| 轴流压气机非设计点性能计算 |
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| 引用本文： | 胡江峰,竺晓程,欧阳华,羌晓青,杜朝辉. 轴流压气机非设计点性能计算[J]. 航空动力学报, 2012, 27(3): 682-688 |
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| 作者姓名： | 胡江峰 竺晓程 欧阳华 羌晓青 杜朝辉 |
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| 作者单位： | 1.上海交通大学 机械与动力工程学院, 上海 200240 |
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| 基金项目： | 国家自然科学基金(51076101/E060203) |
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| 摘 要： | 采用流线曲率法数学模型,结合跨声速轴流压气机的内部流场特征,拓展了一种非设计点特性计算方法.该方法基于近年来的国内外研究进展,考虑了非设计点工况下影响落后角及损失的诸多因素.对轴流跨声速压气机NASA(National Aeronautics and Space Administration)TP1669进行了数值计算,得到了展向参数分布和全工况下性能曲线,通过与实验值的对比和分析证明该方法和模型是可行的,可为压气机设计和优化提供参考.
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| 关 键 词： | 流线曲率法 压气机 非设计点 落后角 损失 |
| 收稿时间： | 2011-04-27 |
| 修稿时间： | 2011-09-07 |
Axial compressor performance calculation at off-design conditions |
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| HU Jiang-feng,ZHU Xiao-cheng,OU YANG Hu,QIANG Xiao-qing and DU Zhao-hui. Axial compressor performance calculation at off-design conditions[J]. Journal of Aerospace Power, 2012, 27(3): 682-688 |
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| Authors: | HU Jiang-feng ZHU Xiao-cheng OU YANG Hu QIANG Xiao-qing DU Zhao-hui |
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| Affiliation: | 1.School of Mechanical Engineering, Shanghai Jiao Tong University, Shanghai 200240, China2.School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China |
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| Abstract: | The axial compressor performance prediction method was developed,based on streamline curvature method,according to the flow mechanics of transonic axial compressor.This method considered the series impacts of deviation and loss to a certain extent according to the national and international openning research progresses.The internal flow field of NASA(National Aeronautics and Space Administration) TP1659 was calculated,thus obtained the span-wise aerodynamic parameters and characteristic curves at design and off-design points.With the comparison between simulation and experimental value,this method and models are validated to be applicable,and can be used for compressor design and optimization. |
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| Keywords: | streamline curvature method compressor off-design deviation loss |
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