...大迎角；细长圆锥前体；非对称分离涡；主动流动控制 [gap=1390]Key words: fluid mechanics; stability of vortices; high angles of attack; slender conical forebody; asymmetrical vortices; active flow control ..
基于14个网页-相关网页
Aeroelastic analysis at high angles of attack is an attractive and complicated research subject in modern aircraft design.
大迎角气动弹性分析是现代飞行器设计中非常引人瞩目并且复杂的研究课题。
The conclusion is that the key to raise the experimental accuracy lies in reducing and correcting the systematic errors due to blockage effect at high angles of attack.
结论是：提高大攻角实验数据准确度的关键在于减少和修正由于阻塞效应引起的系统误差。
The unsteady motion of a two-dimensional thick airfoil at high angles of attack is considered in this paper.
本文研究二维厚度翼型的大攻角非定常运动。
应用推荐