The optimal design of civil aircraft winglet with multiple constraint;
民用飞机翼梢小翼多约束优化设计
The structure of wingtip vortex and the affection of tap on wingtip vortex is investigated in this paper.
本文的研究目的是弄清机翼翼梢涡的结构及安装翼梢扰流片对翼梢涡的影响。
