航空学报 > 1991, Vol. 12 Issue (4): 127-132

纵向静稳定性洞壁干扰修正方法的改进

江桂清   

  1. 中国空气动力研究与发展中心
  • 收稿日期:1990-02-19 修回日期:1990-07-19 出版日期:1991-04-25 发布日期:1991-04-25

AN IMPROVED WALL CORECTION METHOD FOR THE LONGITUDINAL STABILITY

Jiang Guiqing   

  1. China Aerodynamic Research, Development Center
  • Received:1990-02-19 Revised:1990-07-19 Online:1991-04-25 Published:1991-04-25

摘要: 对纵向静稳定性作洞壁干扰修正时,应考虑由于攻角改变平尾在风洞实验段中位置的变化。根据尾翼实际位置确定尾翼处的干扰因子τ。此外,在传统的洞壁干扰修正中,尾翼区段对俯仰力矩系数的贡献效率m_z/a_t常以尾翼效率m_t/φt代替,本文对此作了改进。应甩改进后的洞壁干扰修正方法对实验结果进行了修正,效果良好。

关键词: 洞壁干扰, 风洞实验, 实验技术

Abstract: The variation of horizontal tail position due to the angle of attack should be taken into account when wall-interference corrections on the longitudinal stability are performed. The interference factor at tail,τ,is determined by the actual position of the tail. In addition, in the ordinary wall correction method, the effectiveness of the tail panel (?)mz/(?)t which is contributed to the pitching moment coefficient is usually substituted by .It is corrected in this paper to account for the wall interference by using the improved method, and favourable results are obtained.

Key words: wall-interference, wind tunnel tests, experimental technique