搜索资源列表
wogefa
- 涡格法是空气动力学中的常用方法之一，这个程序可以通过自己设置机翼的节点来调整机翼的网格，设置来流速度，计算机翼的气动力。最后通过计算《空气动力学》教程中的一个涡格法算例验证了程序的正确性
涡格法计算算例2
- 涡格法计算机翼涡强，并且就几个不同参数进行比较分析
HVLL
- 经典螺旋桨设计程序 采用精确度较高的涡格法-propeller design Vortex Lattice method
wogefajisuan
- 涡格法计算机翼的涡强，对不同剖面形状，拱度等进行了比较分析。-Vortex lattice method the computer wing of the vortex is strong, the shape of different profiles, such as camber, a comparative analysis.
wogewoge0
- 涡格法求解翼型的气动力，包括阻力 升力 法向力-Vortex lattice method for solving the the aerodynamic airfoil, including resistance lift normal force
T135_export
- 涡格法计算现行气动力的matlab代码，用于飞机机翼概念设计阶段的气动力评估-Tornado is a Vortex Lattice Method for linear aerodynamic wing design applications in conceptual aircraft design or in aeronautical education
vlmd
- 计算低速气动力的涡格法程序，来自NASA，可信度高-This is a vortex lattice aerodynamic program from the low speed aerodynamics group at NASA Langley
LSver01-(1)
- 利用FORTRAN编写的涡格法计算3D水翼所受升力与阻力的程序-Calculated using the FORTRAN prepared vortex lattice method 3D hydrofoil suffered lift and drag programs
3DHydrofoilCal
- 升力面法计算水翼动力系数，提供给学螺旋桨的朋友(Calculation of dynamic coefficients of hydrofoil by lifting surface method)
涡格法代码
- 涡格法计算机翼的表面的升力和升力系数，采用高斯迭代求解(The lift and lift coefficients on the surface of the computer wings of the vortex lattice are solved by Gauss iteration)
AB
- 非线性涡格法公式编程，用matlab打开(Nonlinear vortex lattice formula programming, open with MATLAB)
涡格法计算升力
- 利用涡格法计算对称机翼的升力，压心和焦点(Calculation of lift force, center of pressure and focus of symmetrical wing by vortex lattice method)