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5 Class E: ROTORCRAFT -An aerodyne that derives the whole or a substantial part of its lift from a rotary wing system.

E 级:旋机—一种重航空器产生的全部或相当大的一部分爬升力﹙ lift ﹚来自从旋系统﹙ rotary wing system ﹚。

TILT ROTORCRAFT : An aerodyne which derives the whole or a substantial part of its lift for vertical or hovering flight by tilting rotor upward to a position substantially vertical, and in forward flight derives its lift from rotors and/or wings, and is capable of autorotation in the event of power failure.

倾斜旋飞机:一种旋机,垂直或悬浮飞行时,整个或其中相当一部分之爬升力源自倾斜旋转使上升到一个极度垂直的位置,而在向前飞行时,爬升力源自旋转和/或机,并有能力在发生动力供应中断时自动旋转。

The inverse method was used in aerofoil of fan blade design, a nonlinear algorithm of velocity distribution optimization, different optimize methods was introduced ,according to the difference of suction and pressure surface, this technique can adjust the thickness of aerofoil available.

使用反方法进行风机叶片的型设计,采用了一种非线性优化速度分布的方法,分别针对吸、压力面的初始速度分布采用不同的优化手段,可以有效地调节型的厚度。

Huge size 7 cases,large size 63 cases,small size 11 cases.the operative approach included revised pterional approach 53 cases,combined subfrontal-pterional approach 7 cases,perional approach with zygomatic arch removal 15 cases,pterional approach together with frontal and temporal approach 6 cases.results simpson grade ⅰ remove was 45 cases;grade ⅱ 12 cases;ⅲa 9 cases;ⅲb 6 cases;ⅳa 3 cases.

巨大型7例,大型63例,小型11例。采用改良点入路53例;额下点联合入路7例;经颧弓点入路15例;额颞眶颧入路6例。结果 simpson ⅰ级切除45例,ⅱ级切除17例,ⅲa级切除9例,ⅲb级6例,ⅳa级3例。

The operative approach included revised pterional approach 53 cases,combined subfrontal-pterional approach 7 cases,perional approach with zygomatic arch removal 15 cases,pterional approach together with frontal and temporal approach 6 cases.

采用改良点入路53例;额下点联合入路7例;经颧弓点入路15例;额颞眶颧入路6例。

Make sure the shape of the wing, especially if it is going downwards, is not conflicting with the gears ( if the wing's minimum Z coordinate is lower than the gear's, that means that when landed on the ground, the wing tip will be under the ground !).

要注意的外形,尤其如果它是朝下的,那不能与着起落架矛盾(如果的最小Z坐标低于起落架,那意味着当船着陆时,尖会戳进地面中!)。

Example: Turning right, the right tip of the wing goes down and the left side is goes up, thus we rotate about an axis through the center of the wing.

向右旋时,右侧的端会向下沈,左侧的端则会向上升,因此我们会沿著伞中心的轴线旋动。

A calculated model for predicting wing download of the tiltrotor in hover and forward flight was given according to the aerodynamic interaction effect of the rotor downwash flow on the wing.

该模型中,旋在机处产生的诱导速度以及对机干扰的旋尾迹边界基于Weissinger-L升力面理论和自由尾迹方法计算,以考虑倾转旋桨叶的大负扭转和尖削带来的较大三维影响,机表面流则区分为弦向流及展向流,以分别计算向下载荷。

In order to calculate the helicopter hover ceiling in OGE precisely, some aerodynamic parametem, such as tip loss effect, induced velocity distribution, the effect of rotor downwash on the fuselage and power transfer of engine into rotor, must be treated carefully.

准确计算直升机的悬停升限依赖于诸如桨尖损失系数,非均匀旋诱导速度分布,旋下洗引起的直升机增重效应及发动机与旋之间的功率传递系数等气动参数的准确度。

The result exhibit add flutter better than no flutter, especially MDF on 1k~1.25 kHz and Japanese cedar on 1.6 kHz could get the best scattering coefficients S=1, even on 5kHz still have the scattering effect.

本研究进一步探讨有、无板对扩散板散射效果之影响,分别以三组不同木质材料进行比较,结果显示,有板之散射效果比无板佳,其中又以MDF 於1k~1.25kHz与柳杉於1.6kHz时有最佳之散射效果S=1,且於最高频5kHz时仍有散射效果产生。

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