attack angle发音

意思翻译

攻角；[测]迎角；[机]冲角

相似词语短语

attack───vt.攻击；抨击；动手干；vi.攻击；腐蚀；n.攻击；抨击；疾病发作；n.(Attack)人名；(瑞典)阿塔克

angle───n.角，角度；视角；立场；角铁；（古）鱼钩；v.斜移；从……角度提供信息；钓鱼；谋取

shark attack───[电影]水深火热之生化狂鲨；鲨鱼攻击；生化狂鲨（电影名）

asthma attack───哮喘发作（歌曲名，AsthamAttack）

nuclear attack───核攻击；核袭击

air attack───n.空袭

slanderous attack───诽谤性攻击

frap attack───frap攻击

insect attack───[植保]虫害

双语使用场景

While for small clearance, there appear repulsion phenomena, and the variation of coefficients with attack Angle is nonlinear.───当物体离壁面很近时，出现排斥现象，水动力系数随攻角的变化呈非线性特征。

The torsion reduces the effectual attack angle of the elastic sweep wing.───角的减小又使得弹性机翼的有效气动力载荷减小。

effect of initial attack angle and pitching angular velocity on the selection of release angle is remarkable.───得到标枪的初始攻角和俯仰角速度对出手角度选择的影响较显著。

The attack angle the bomber comes in at is critical, since the bomber attacks in a straight line.───由于轰炸机的攻击是直线的，所以它的攻击角度是很重要的。

The penetration depth decreases with the increase of initial attack angle at the same velocity, which appears a linear relationship.───相同速度下，随着初始攻角的增大侵彻深度变小，基本呈线性关系。

Its object is to design the pitch program for a missile by giving attack angle program.───其目的是根据给定导弹的攻角方案设计其俯仰角方案。

When flapping-wing flight at small attack angle, wing had wing-blade improve effectively aerodynamic characteristic of flapping-wing.───当扑翼在小迎角飞行时，机翼带翼刀可以有效地改善扑翼的气动特性。

The guidance and control system is properly designed and can meet the accuracy and attack angle requirement for still or mobile target.───制导控制系统设计合理，对于静止和机动目标，落点射击精度和落角均满足设计要求。

The advantage of extended penetrator is obvious at high velocity or little attack angle.───结果表明：当攻角小或速度大时，伸出式侵彻体相对基准杆有较明显的优势；

英语使用场景

While impulse forces not acting on the centroid, the influence of accessional attack angle oscillation amplitude, impulse force scale and function time interval on range correction was discussed.

The paper has introduced design of the support system for rotary balance of high attack angle, and the importance and methods of studying spin of aircraft.

The methods are devoted to determining aerodynamic performances for asymmetrical body with angle of attack, angle of side slip and roll angle.

With the increase of attack angle, the transiton point moves from the frailing edge to leading edge.

If the advantaged opportunity is chosen, the oscillation of accessional attack angle may be reduced greatly. So the effect would be close to the expecting revision result while acting on the centroid.