摘要
本文建立了可控翼伞气动力计算的等效翼型—柔性模型以及雀降操纵力计算的双体铰接模型。用曲面涡格法对翼伞的气动力进行了计算，在此基础上，对翼伞的雀降操纵力也进行了计算。
In this paper, the “equivalent airfoil flexible model” for the aerodynamic calculation and the “two body hinged model” for the flare control force calculation of a parafoil is established. The aerodynamics of the parafoil is calculated by using the nonplane vortex grid method. On the basis of these calculation results, the flare control force is calculated.
出处
《国防科技大学学报》
EI
CAS
CSCD
1999年第3期21-24,共4页
Journal of National University of Defense Technology
