1) separated flow of high angle of attack
大攻角分离流
2) large incidence separation flow
大攻角分离流动
5) flow characteristics at a large incidence
大攻角流动特性
6) large attack angle
大攻角
1.
The frequency of oscillating excitation has more effect on improving aerodynamic performance of airfoil at large attack angle th.
利用振荡扰流进行了改善风力机翼型大攻角下性能的研究。
2.
This paper presents a numerical simulation of separated flow over an airfoil at large attack angles with oscillating excitations to study separation flow control over an airfoil.
为了研究大攻角下振荡射流控制翼型流动分离的机理,应用基于有限体积法和压力修正的SIMPLEC算法,数值模拟了表面施加振荡射流的翼型分离流动。
3.
Based on the characteristics of the complicated aerodynamics for the large attack angle air-to-air missile,using feedback linearization approach for the design of the flight control system is proposed.
针对大攻角空空导弹飞行过程中复杂的非线性空气动力学特性,提出了采用反馈线性化进行控制器设计的方法。
补充资料：临沂战役(见山东军区大反攻)
临沂战役(见山东军区大反攻)
Linyi, Battle of
Linyi ZhQnyi临沂战役(l一ilayi，Battlc川抗日，l戈争-时期，八路场广山东军区所属角一}，、滨海军区部队各1部对驻临沂县城伪‘/l::l，l{]进攻战役，歼火伪下2 00()余人解放J’ll介沂城。见山东军区大反攻
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条