航空学报 > 1990, Vol. 11 Issue (12): 523-527

高速风洞洞壁干扰和支架干扰的工程修正方法

崔乃明   

  1. 中国空气动力研究与发展中心
  • 收稿日期:1988-05-27 修回日期:1990-04-04 出版日期:1990-12-25 发布日期:1990-12-25

AN ENGINEERING CORRECTION METHOD FOR TUNNEL WALL INTERFERENCE AND STING-SUPPORT INTERFERENCE IN HIGH SPEED WIND TUNNELS

Cui Naiming   

  1. China Aerodynamic Research and Development Center
  • Received:1988-05-27 Revised:1990-04-04 Online:1990-12-25 Published:1990-12-25

摘要: 本文采用涡格法作为洞壁干扰和支架干扰的修正方法,该方法需要知道包含在高速风洞通气壁边界条件中的透气性参数Q。应用理论计算配合实验的方法确定了FL-21风洞的洞壁特性曲线Q~Ma,洞壁特性参数Q在亚音速时随Ma数增加而增加。文中应用该曲线对一些实验结果进行了洞壁干扰和支架干扰修正,所得结果与国外计算值和国内实验值吻合较好。

关键词: 开缝壁, 洞壁干扰修正, 跨音速风洞

Abstract: This article presents a method to correct tunnel wall and support interferences based on vortex lattice method. The method needs to know the porosity parameter Q involved in the boundary condition of ventilated wall in the high speed wind tunnel. FL-21 wind tunnel wall characteristic curve Q-Ma is determined by combining computations with experiments. Q increases with Ma in subsonic speeds. According to the curve some test data are corrected for tunnel wall and support interferences. The corrected results agree -well with those attained from theories published abroad and from experiments obtained at home.

Key words: Slotted walls, wall interference correction, transonic wind tunnels.