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1)  stall and large attack angle
过失速大迎角
1.
Under the conditions of stall and large attack angle,normal effectors lose their manoeuvre capability.
过失速大迎角飞行条件下,常规舵面失去了操纵能力,需要开发新型控制律算法来研究推力矢量和推力对飞行性能的影响。
2)  high-angle-of-attack/post-stall agility
大迎角/过失速敏捷性
3)  stall-incidence
失速迎角
1.
The effects of elastic vibrations on the flow fields near the stall-incidence of the airfoil are investigated.
通过求解雷诺平均Navier-Stokes方程得到气动力,结合翼型振动方程,计算了翼型不同迎角下的动态过程,分别通过层流和湍流情况的计算,重点研究了弹性振动对翼型失速迎角附近流场的影响,研究结果表明,在中低雷诺数、翼型具有弹性振动的情况下,翼型的失速迎角会比传统定常意义上的失速迎角提前出现,为长期以来数值计算得到的失速迎角与风洞实验、飞行试验结果的不同给出了一种物理解释。
4)  transonic high-incidence flows
跨声速大迎角流动
5)  high angle of attack
大迎角
1.
Investigation on the interference of rear sting supports at high angle of attack in low speed wind-tunnel;
低速大迎角尾撑支架干扰试验研究
2.
Study on high angle of attack test technique of rear sting supports;
尾撑大迎角试验技术研究
3.
Investigation of improving the lateral static stability for the aircraft applied to high-subsonic flow and high angle of attack;
某型飞机高亚声速大迎角横向静稳定性改善研究
6)  high angles of attack
大迎角
1.
Primal research of the effect of flow turbulence on aerodynamic characteristics of a aircraft model at high angles of attack;
湍流度对飞行器模型大迎角气动特性影响的初步研究
2.
Effects of grit strip on flow asymmetry over a slender revolution body at high angles of attack;
粗糙带对细长体大迎角流动非对称性的影响
3.
An investigation on the effect of the acoustic excitation on flow asymmetry over a slender revolution body at high angles of attack in compressible flows;
可压缩流中声激励对细长体大迎角流动非对称性的影响研究
补充资料:河阳石尚书破回鹘、迎贵主、过上党射鹭鶿,
【诗文】:
塞北虏郊随手破,山东贼垒掉鞭收。乌孙公主归秦地,
白马将军入潞州。剑拔青鳞蛇尾活,弦抨赤羽火星流。
须知鸟目犹难漏,纵有天狼岂足忧。[尚书将入潞府,偶逢水鸟鹭鸶,引弓射之,一发中目,三军踊跃,其事上闻,诏下美之。]画角三声刁斗晓,
清商一部管弦秋。他时麟阁图勋业,更合何人居上头。



【注释】:
【注释】:
原题:河阳石尚书破回鹘、迎贵主、过上党射鹭鶿,绘画为图,猥蒙见示,称叹不足,以诗美之


【出处】:
全唐诗:卷460-35
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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