纳卡0012 翼型(Naca 0012 Airfoil) 作品集:3D模型_G388284套 James_Walker 4个月前 纳卡-6412-翼型-1(naca-6412-airfoil-1) 作品集:3D模型5834套 唯_344 5个月前 纳卡-64A.203-翼型-1(naca-64a203-airfoil-1) 作品集:3D模型5834套 唯_344
Airfoil design The airfoil's geometry was designed using a CAD software, SolidWorks. The NACA 0012 airfoil's basic shape was used as a base, and a circular dent of 30 mm depth was added to the upper surface of the airfoil. The airfoil's chord length was 1 m, and the span was 0.3 ...
3、efined-Functions-Complied 此时打开了 Complied UDFs的窗口,Add在选择UDF的对话框中找到NACA0012D文件夹中 的 airfoil.c文件,选中,ok;此时返回到Complied UDFs的窗口点击Build , FLUENT开始 进行编译, 可以在FLUENT窗口看到编译的一些过程提示;等编译完成,点击Load;就将已经编译好的UDF力口载到FLUENT中了。4) ...
5711 1 35:45 App naca 0012翼型6°攻角风洞模型 2.5万 8 01:22:12 App NACA0018-2D机翼建模与Fluent计算 989 2 14:02 App 02_NACA_N4412翼型fluent计算模型验证 1.0万 0 44:39 App ANSYS 翼型分析 - NACA Airfoil - TUTORIAL 1.5万 0 08:48 App 翼型Solidworks建模步骤 9571 1 14:24 App Fluent ...
The airfoil was designed in the environment of Solidworks, and the CFD analysis was conducted in ANSYS Fluent environment. Results show that the modified airfoil model gives better performance with an increase of turbulence. However, an increase of lift coefficient is not as significant as the ...
SolidWorks-2018 program was used to model the system of the wing parts, which consists of seven ribs and two spars and airfoil NACA 0012 was used and aluminum alloy T7075 as a material for the structure of the aircraft wing and its surface. The generated loads were projected on ...
纳卡0012 翼型(NACA0012 Airfoil) 作品集:3D模型_G100套 James_Walker 2个月前 参数NACA-4 翼型(Parametric NACA-4 Airfoil) 作品集:3D模型_G100套 James_Walker 2个月前 纳卡24012 翼型3三维设计(NACA24012 Airfoil 3D Design) 作品集:3D模型_G100套 ...