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vpm
- 二维涡流位置及流场分布计算程序,Vortex Panel Method
2d-airfoil-release2.0
- 2d-airfoil-release2.0,解2维机翼的面元法,运行时放在英文目录下-2d-airfoil-release2.0, solutions of two-dimensional wing panel method, the runtime directory in English
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.
surface
- 运用面元法结合牛顿理论进行高超声速飞行器气动力工程估算(The aerodynamic engineering estimation of hypersonic vehicle is carried out by using the panel method and Newton theory)