首页 | 本学科首页   官方微博 | 高级检索  
     

带跨音结尾激波的二元收-扩管内附面层控制实验研究
引用本文:何中伟. 带跨音结尾激波的二元收-扩管内附面层控制实验研究[J]. 推进技术, 1988, 9(6): 24-30,70
作者姓名:何中伟
摘    要:本文较深入地研究了由直-曲壁构成的二元收-扩管内收敛段底壁的附画层抽气板形状,在吸除系数为1条件下,吸除附面层对几何喉道附近壁画、对跨音结尾激波与扩压器壁附面层干扰区上游的附面层发展的影响;研究了结尾跨音激波与扩压器底壁附面层干扰区的附面层控制对其下游的流场畸变的影响;文中并对有、无附面层控制下的干扰区下游的动态畸变作了比较.指出,通过对干扰区的附面层抽吸,近壁面的紊流度峰值和平均值大大下降.

关 键 词:进气道  边界层控制  激波干扰  流场畸变

EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER CONTROL OF TWO-DIMENSIONAL CONVERGENT-DIVERGENT DUCT WITH TERMINAL TRANSONIC SHOCK-WAVE
He Shongwe. EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER CONTROL OF TWO-DIMENSIONAL CONVERGENT-DIVERGENT DUCT WITH TERMINAL TRANSONIC SHOCK-WAVE[J]. Journal of Propulsion Technology, 1988, 9(6): 24-30,70
Authors:He Shongwe
Abstract:On condition that CQ =1, the effects of boundary-layer suction in the bottom of convergent region of the two-dimensional convergent-divergent duct on boundary-layer development on the wall near the throat and upstream interaction region between the transonic wave and the boundary-layer are studied in more detail in this paper.The effects of boundary-layer control of the interaction region between the transonic shock-wave and boundary-layer on the bottom wall of the divergent section on the flow distortion of the downstream interaction region are also investigated.The flow dynamic distortion of the downstream interaction region with and without boundary-layer control is presented, and it is pointed out that by means of boundary-layer suction in the interaction region the peak turbulence near the bottom wall and its average value are apparently reduced.
Keywords:Inlet  Boundary layer control  Shock wave refelction   Flow distortion  
本文献已被 CNKI 等数据库收录!
点击此处可从《推进技术》浏览原始摘要信息
点击此处可从《推进技术》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号