vertical tail中文,vertical tail的意思,vertical tail翻译及用法

2025-11-02 02:08 浏览次数 12

vertical tail

英[ˈvə:tikəl teil]美[ˈvɚtɪkəl tel]

[航] 垂直尾翼

vertical tail 英语释义

英语释义

  • the vertical airfoil in the tail assembly of an aircraft

vertical tail 片语

片语

VT Vertical Tail垂直尾翼

lower vertical tail垂直尾翼

upper vertical tail上垂直尾翼

vertical tail unit垂直尾翼组

vertical tail surface垂直尾面

vertical stabilizer(美)垂直尾翼

twin-vertical tail双垂尾

VTP Vertical Tail Plane垂直尾翼平面

aircraft vertical tail飞机垂尾

Vertical Tail Model垂直尾翼模型

vertical tail 例句

英汉例句

  • the invention discloses a system and a method for dotting level survey dots of wings and a vertical tail of an airplane.

    本发明公开了一种飞机机翼、垂尾水平测量点的打制系统及方法。

  • it uses the same j-85 engine as its propulsion system but has a twin, outwardly canted vertical tail similar to the boeing f/a-18.

    它使用相同的j-85发动机当做它的动力但是双发飞机,机身上的倾斜垂尾类似波音f/a-18。

  • high aspect-ratio flying wing configurations usually use split-drag-rudder(sdr) and a set of elevons to fulfill the lateral-directional control, without the traditional vertical tail and rudder.

    大展弦比飞翼构型取消了垂尾和方向舵,通常采用开裂式方向舵和多组升降副翼组合来实现滚转和偏航操纵。

  • the high-aspect-ratio flying wing eliminates vertical tail and conventional rudder, and uses instead a split drag rudder with large deflection as its directional control surface.

    大展弦比飞翼布局飞机取消了垂尾和常规方向舵,通常采用大偏角的开裂式方向舵作为偏航操纵面。

  • double-wing micro air vehicles adopts the aerodynamic shape: no tail , only wings and vertical tail placing in wing.

    双翼式微型飞行器采用无尾式,且只有机翼,垂尾也置于机翼上的气动布局。

  • the vertical tail size is not set to avoid spiral instability because this mode is not critical.

    垂尾的大小不是根据避免螺旋不稳定来确定的。因为这种运动模态不是设计状态。

  • the aircraft features an all-flying vertical tail (rudder) section for excellent effectiveness and control, especially at low speeds.

    该机采用了全优的成效飞行垂直尾翼和控制(方向舵)节,尤其是在低的速度。

  • the feasibility of the method proposed is verified by the aerodynamic data of a certain type of native airplane with v-shape vertical tail in flight balance state.

    结合国内某型号飞机含有v型垂尾在配平时的数据验证算法正确性。

  • the drag reduction caused by separation weakening on vertical tail results in drag increasing slowly with the increase of the positive attack angle.

    垂尾分离随迎角增加而不断减弱,从而导致正常式布局后体阻力随迎角变化表现为非对称。

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