翼型伞力矩特性风洞试验研究

PARAFOIL AERODYNAMIC MOMENT CHARACTERISTICS RESEARCH THROUGH WIND TUNNEL TEST

本文介绍在8m×6m低速风洞中进行的某研究型冲压式翼平力矩特性试验研究。给出试验方法及其典型的试验结果。通过应用这一风洞试验技术，可为翼型伞设计提供其他试验手段以得到的翼伞操稳特性气动参数。

In this paper, the testing study of a type of parafoil's aerodynamic moment characteristics in CARDC 8m×6m low speed wind tunnel is introduced. The test methods and some typical results are presented. Using This new wind tunnel test technique can aquire the stability and control aerodynamic parameters of a developing or new designed parafoil. These data are difficult to be aquired through other methods.