attack angle的意思

attack angle中文翻譯：

攻角；[測]迎角；[機]沖角

相似詞語短語

attack───vt.攻擊；抨擊；動手干；vi.攻擊；腐蝕；n.攻擊；抨擊；疾病發作；n.(Attack)人名；(瑞典)阿塔克

angle───n.角，角度；視角；立場；角鐵；（古）魚鉤；v.斜移；從……角度提供信息；釣魚；謀取

shark attack───[電影]水深火熱之生化狂鯊；鯊魚攻擊；生化狂鯊（電影名）

asthma attack───哮喘發作（歌曲名，AsthamAttack）

nuclear attack───核攻擊；核襲擊

air attack───n.空襲

slanderous attack───誹謗性攻擊

frap attack───frap攻擊

insect attack───[植保]蟲害

雙語使用場景

While for small clearance, there appear repulsion phenomena, and the variation of coefficients with attack Angle is nonlinear.───當物體離壁面很近時，出現排斥現象，水動力系數隨攻角的變化呈非線性特征。

The torsion reduces the effectual attack angle of the elastic sweep wing.───角的減小又使得彈性機翼的有效氣動力載荷減小。

effect of initial attack angle and pitching angular velocity on the selection of release angle is remarkable.───得到標槍的初始攻角和俯仰角速度對出手角度選擇的影響較顯著。

The attack angle the bomber comes in at is critical, since the bomber attacks in a straight line.───由于轟炸機的攻擊是直線的，所以它的攻擊角度是很重要的。

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，隨著初始攻角的增大侵徹深度變小，基本呈線性關系。

Its object is to design the pitch program for a missile by giving attack angle program.───其目的是根據給定導彈的攻角方案設計其俯仰角方案。

When flapping-wing flight at small attack angle, wing had wing-blade improve effectively aerodynamic characteristic of flapping-wing.───當撲翼在小迎角飛行時，機翼帶翼刀可以有效地改善撲翼的氣動特性。

The guidance and control system is properly designed and can meet the accuracy and attack angle requirement for still or mobile target.───制導控制系統設計合理，對于靜止和機動目標，落點射擊精度和落角均滿足設計要求。

The advantage of extended penetrator is obvious at high velocity or little attack angle.───結果表明：當攻角小或速度大時，伸出式侵徹體相對基準桿有較明顯的優勢；

英語使用場景

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.