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1)  ta ying
大迎
2)  Nei Da Ying
内大迎穴
1.
Clinical Observation on the Method of Needling Nei Da Ying Channal for treatment of Tongue Dyskinesia Post-stroke;
针刺内大迎穴治疗中风后舌体运动障碍的疗效观察
2.
Objection: To observe the therapeutic effect of needling "Nei Da Ying" on Tongue Dyskinesia Post-stroke, and analyse the clinical correlated factors of therapeutic effect on this acupuncture therapy.
目的:观察针刺内大迎穴治疗中风后舌体运动障碍的疗效,同时探讨临床相关因素对疗效的影响。
3)  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
4)  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
5)  high AOA
大迎角
1.
J7L high AOA/stall/spin flight test;
J7L飞机大迎角/失速/尾旋试飞
2.
In this paper, the importance or necessity for the installation and employment of an anti spin parachute system for the flight test research on modern aircraft high AOA characteristic, especially for the stall/spin and post stall flight test, is described briefly.
简要介绍了研制与安装应急反尾旋伞系统对现代高机动飞机的大迎角特性试验研究的重要作用 ,特别是对失速 /过失速 /尾旋特性试验鉴定的必要性和重要性。
6)  maximum angle of attack
最大迎角
补充资料:大迎

大迎

大迎   经穴名。出《素问·气穴论》。别名髓孔。属足阳明胃经。在面部,下颌角前方咬肌附着部前缘,当面动脉搏动处。布有面神经及颊神经,前方有面动、静脉通过。主治齿痛,颊肿,牙关紧闭,口,及面神经麻痹,腮腺炎等。斜刺0.3-0.5寸,或沿皮刺0.5-1寸,避开血管。艾条灸3-5分钟。

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