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avl3.31
- Drale编写的升力面模型，机翼表面被离散为涡格。与升力线模型相比，升力面模型更多的考虑了机翼的几何形状。-Lifting surface model Drale write the wing surface the discrete vortex lattice. Compared with the lifting line model, the lifting surface model consideration of the g
pablo
- 国外使用面元法计算翼型升力的matlab程序包-matlab program using panel method to solve the lift of the foil
DLM
- 计算升力面非定常气动力的偶极子网格法MATLAB程序-Matlab functions to calculate unsteady aerodynamic pressures on a lifting surface using doublet lattice method.
mian
- 利用牛顿面元法计算飞行器的升力、阻力、俯仰力矩等。-Calculation of the aircraft lift, drag, pitching moment, etc. Newton panel method.
AIC-matrix
- 偶极子法计算振动翼面升力分布的源码，根据文中介绍的方法编程来的-Dipole method to calculate the vibration of the airfoil lift distribution of the source code, according to the method described in the article programming to
Caculation-for-NACA24012
- 程序包二维翼型，计算涡面元系数，画出翼型，压力系数，升力系数，并在来流速度为1的时候画出翼型上下表面的速度-Caculation for airfoil including
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)
升力面
- 矩形水翼使用升力面方法进行计算的程序，matlab编程。包含均匀网格和余弦网格两种分格方法。(The rectangular hydrofoil is calculated using the lifting surface method, and the program is programmed by matlab. Two grid methods including uniform mesh and cosine mesh.)