我們要根據(jù)大型飛機(jī)模型的不同用途去選擇不同的翼型。翼型很多，好幾千種。但歸納起來(lái)，飛機(jī)的翼型大致分為三種。

We need to select different airfoils according to different uses of large aircraft models. There are many kinds of airfoils. But to sum up, there are roughly three types of aircraft airfoils.

一是平凸翼型，這種翼型的特點(diǎn)是升力大，尤其是低速飛行時(shí)。不過(guò)，阻力中庸，且不太適合倒飛。這種翼型主要應(yīng)用在練習(xí)機(jī)和像真機(jī)上。二是雙凸翼型。其中雙凸對(duì)稱(chēng)翼型的特點(diǎn)是在有一定迎角下產(chǎn)生升力，零度迎角時(shí)不產(chǎn)生升力。飛機(jī)在正飛和到飛時(shí)的機(jī)頭俯仰變化不大。

One is the planoconvex airfoil, which is characterized by high lift, especially at low speed. However, the resistance is moderate and is not suitable for inverted flight. This kind of airfoil is mainly used in training machines and video cameras. The second is the biconvex airfoil. The characteristic of the biconvex symmetric airfoil is that it produces lift at a certain angle of attack and does not produce lift at zero angle of attack. The nose pitch of the aircraft does not change much when it is flying and when it is arriving.

這種翼型主要應(yīng)用在特技機(jī)上。三是凹凸翼型。這種翼型升力較大，尤其是在慢速時(shí)升力表現(xiàn)較其它翼型優(yōu)異，但阻力也較大。這種翼型主要應(yīng)用在滑翔機(jī)上和特種飛機(jī)上。另外，機(jī)翼的厚度也是有講究的。同一個(gè)翼型，厚度大的低速升力大，不過(guò)阻力也較大。厚度小的低速升力小，不過(guò)阻力也較小。實(shí)際上就選用翼型而言，它是一個(gè)比較復(fù)雜、技術(shù)含量較高的問(wèn)題。其基本確定思路是：根據(jù)飛行高度、翼弦、飛行速度等參數(shù)來(lái)確定該飛機(jī)所需的雷諾數(shù)，再根據(jù)相應(yīng)的雷諾數(shù)和您的機(jī)型找出合適的翼型。還有，很多真飛機(jī)的翼型并不能直接用于模型飛機(jī)，等等。這個(gè)問(wèn)題在這就不詳述了。

This airfoil is mainly used in aerobatics. The third is concave and convex airfoil. The lift of this airfoil is large, especially at slow speed, which is superior to other airfoils, but the drag is also large. This airfoil is mainly used in gliders and special aircraft. In addition, the thickness of the wing is also exquisite. For the same airfoil, the lift at low speed with large thickness is large, but the drag is also large. The low-speed lift with small thickness is small, but the resistance is also small. In fact, the selection of airfoil is a relatively complex and technical problem. The basic idea is to determine the required Reynolds number of the aircraft according to the flight height, wing chord, flight speed and other parameters, and then find the appropriate airfoil according to the corresponding Reynolds number and your model. Also, many real aircraft airfoils cannot be directly used for model aircraft, and so on. This problem will not be detailed here.

機(jī)翼常見(jiàn)的形狀又分為：矩形翼、后掠翼、三角翼和紡錘翼（橢圓翼）。

The common shapes of wings are divided into rectangular wing, swept wing, delta wing and spindle wing (oval wing).

矩形翼結(jié)構(gòu)簡(jiǎn)單，制作容易，但是重量較大，適合于低速飛行。后掠翼從翼根到翼梢有漸變，結(jié)構(gòu)復(fù)雜，制作也有一定難度。后掠的另一個(gè)作用是能在機(jī)翼安裝角為0度時(shí)，產(chǎn)生上反1-2度的上反效果。

The rectangular wing is simple in structure and easy to make, but it is heavy and suitable for low speed flight. The swept wing has a gradual change from the wing root to the wing tip, and its structure is complex, so it is also difficult to make. Another function of the sweep back is to produce an up-reflection effect of 1-2 degrees when the wing installation angle is 0 degrees.

三角翼制作復(fù)雜，翼尖的攻角不好做準(zhǔn)確，翼根受力大，根部要做特別加強(qiáng)。這種機(jī)翼主要用在高速飛機(jī)上。

The manufacturing of delta wing is complex, the attack angle of wing tip is not easy to be accurate, and the force on wing root is large, so the root should be specially strengthened. This kind of wing is mainly used in high-speed aircraft.

紡錘翼的受力比較均勻，制作難度也不小，這種機(jī)翼主要用在像真機(jī)上。翼梢的處理。

Spindle wings are uniformly stressed and difficult to make. This kind of wing is mainly used in video cameras. Treatment of wing tip.

由于機(jī)翼下面的壓力大于機(jī)翼上面的壓力，在翼梢處，從下到上就形成了渦流，這種渦流在翼梢處產(chǎn)生誘導(dǎo)阻力，使升力和發(fā)動(dòng)機(jī)功率都會(huì)受到損失。為了減少翼梢渦流的影響，人們采取改變翼梢形狀的辦法來(lái)它。更多相關(guān)飛機(jī)模型的事項(xiàng)就來(lái)我們網(wǎng)站http://elongconsult.com咨詢(xún)吧！

Since the pressure below the wing is greater than the pressure above the wing, vortex is formed at the wing tip from bottom to top. This vortex produces induced drag at the wing tip, causing loss of lift and engine power. In order to reduce the influence of wingtip vortex, people take the method of changing the shape of wingtip to solve it. For more matters related to aircraft model, please visit our website http://elongconsult.com Ask!