| 进口为均匀剪切流的二元亚音扩压器 |
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| 引用本文： | 黄熙君,董金钟,范世兴,肖承恕.进口为均匀剪切流的二元亚音扩压器[J].航空动力学报,1988,3(3):235-238,283. |
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| 作者姓名： | 黄熙君 董金钟 范世兴 肖承恕 |
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| 作者单位： | 北京航空航天大学
(黄熙君，董金钟，范世兴)，北京航空航天大学(肖承恕) |
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| 摘 要： | 本文在主流为均匀流的二元亚音扩压器流动计算方法的基础上,发展了一种进口为均匀剪切流的二元亚音扩压器流动特性计算方法。为验证本方法,计算了三种实例,并和试验测定结果进行了比较,二者符合情况良好。
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| 收稿时间： | 1987/10/1 0:00:00 |
TWO-DIMENSIONAL SUBSONIC DIFFUSER FLOW WITH UNIFORM SHEAR VELOCITY PROFILE AT INLET |
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| Huang Xijun,Dong Jinzhong,Fan Shixin and Shao Chengshu.TWO-DIMENSIONAL SUBSONIC DIFFUSER FLOW WITH UNIFORM SHEAR VELOCITY PROFILE AT INLET[J].Journal of Aerospace Power,1988,3(3):235-238,283. |
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| Authors: | Huang Xijun Dong Jinzhong Fan Shixin and Shao Chengshu |
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| Institution: | Beijing Institute of Aeronautics and Astronautics;Beijing Institute of Aeronautics and Astronautics;Beijing Institute of Aeronautics and Astronautics;Beijing Institute of Aeronautics and Astronautics |
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| Abstract: | A prediction method has been developed for average parameters of 2-D subsonic diffuser with uniform shear velocity profile at inlet. A complete solution of all flow parameters can be obtained by interacting the zonal models and coupling them on common boundaries. The momentum integral and the entrainment equations are used for the boundary layer zone. The equations are closed by use of the improved Cole's wall-wake velocity profile. Due to different development of the boundary layers on the upper and lower walls of diffuser under conditions of the shear velocity profile in core flow, different equations are employed. Three actual diffusers are calculated by this method and experimented by authors. The predictions by this method for the streamwise distribution of pressure coefficient, velocity of core flow and the location of detachment are in good agreement with test data. |
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