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Angle of attack typically ranges from 3o to 12o for a paraglider. 典型的飞行伞攻角范围由3度到12度之间。
The existence of angle of attack reduces the inlet performance. 攻角的存在也在一定程度上降低了进气道性能。
effective angle of attack 有效迎角
Jigs for ailerons and tail angles of attack. 用以保证副翼及尾翼安装角的夹具。
The thickness ratio appeared to have little effect on lift coefficient at zero angle of attack, since the angle of zero lift was largely determined by the airfoil camber. 在迎角为零时，由于零升力主要由机翼中弧线决定，相对厚度对升力几乎没有影响。
As seen above, the design angle of attack for the second segment is 10 deg. 如上所述;设计攻角的第二部分是10甘醇.
As seen above, the design angle of attack for the second segment is10 deg. 如上所述;设计攻角的第二部分是10甘醇.
The wind tunnel tests show that long protrusions have little effect on longitudinal aerodynamic characteristics, but a considerable effect on the roll moment especially at a large angle of attack. 经风洞试验了解并证实,长鼓包对纵向气动特性影响不大,对滚转力矩稍有影响,特别是当攻角较大时,对滚转力矩有一定影响。
The conventional tail must be at a negative angle of attack, and the Canard tail at a positive angle. 通常的尾翼必须处于负迎角，而鸭式尾翼则为正迎角。
It indicated a mismatch in the lower-level comparison in the air data system, specifically with angle of attack. 这表明在大气数据系统在比较基准方面有匹配不当的问题，特别是在迎角状态下。
The commander chalked out his plan of attack. 司令官对进攻计划作了粗略的介绍。
His fleet emerged from superluminal at just the correct angle of attack, in good formation and proper deployment. 他的舰队从超光速状态出现到这个位置，攻击角度恰好正确，队形完好，部署适当。
She hit her knee against the angle of the bed. 她的膝盖撞到床角上了。
Effective angle of inner friction 有效内摩擦角
This occurs at one angle of attack for the same wing loading of a paraglider (or any aircraft). 这种情形会发生于飞行伞（或任何的航空器）的翼负载相当于攻角时。
The angle of attack of the submunition doesn't play a role in the aerodynamic interference. 子弹的攻角对气动干扰影响不大；
Because of the effect of an ablation lag the roll torgue is produced when the blunt nosed cones at angles of attack roll relative to the wind fixed coordinates. 当有迎角钝锥相对于风坐标转动时，由于烧蚀滞后效应将产生滚转力矩。
High angle of attack wind tunnel test techniques is necessary for development of high-maneuverability flight vehicles. 大迎角风洞试验技术是先进高机动飞行器研制必需的关键技术。
As the glider turns through half a rotation, its airspeed is slowed down and the angle of attack increased as the pilot starts to pendulum underneath. 当飞行伞经过半圈迴转，它的空速慢下来而攻角加大；同时飞行员开始向下摆盪。
They went in fear of attack by marauding bands. 他们提心吊胆生怕遭到劫匪的袭击。