搜索资源列表
三角面元矩量法
- 电磁场计算的矩量法论文-electromagnetic field of papers Moment Method
pablo
- 面元法计算机翼气动参数,有nasa上百个翼型库文件,可以手动加载,进行翼型设计时可以选择和profile配合使用-pablo
panair
- PANAIR程序源代码(高阶面元法程序) PANAIR程序源代码(高阶面元法程序),在ubuntu11.10中使用fortran编译,能够通过。 (在编译时,PIVC.f90程序中,241行需要修改,去掉一个括号) -PANAIR source code (high order boundary element method program) PANAIR source code (high order boundary element method program) f
mianYuanFa
- 基于面元法的鱼类表面压力以及速度的统计,工程中用高斯列元法进行方程组的求解,结果的显示是使用opencv来实现-hello world!!!
test
- *文件名称: EFIERWGTriangle.cpp *文件标识: *文件摘要:本程序用于计算自由空间平面波入射三角面元剖分的理想导体目标,计算方法是基于电场积分方程和RWG基函数上的矩量法。-The programe is calculate the RCS of PEC using RWG character function
aero
- 面元法程序Module: aero.f -Panel method program-Module: aero.f
Panel-method
- 面元法程序Module: aero.f -Panel method program-Module: aero.f
panel
- 本程序是面元法,主要为了求解绕翼型速度分布。-panel method calculate velocity distribution
pannel-element-method
- 有关流体域的面元法程序,尤其对于解决船舶类运动等有关问题。-Panel element method program in fluid domain,Solving the problem, especially for ship motion.
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
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
panel-method
- 面元法求解三维流场(翼身组合体,高超飞行器),对流场求解结果与实验吻合非常好-An efficient method for solving the three-dimensional flow field-panel method
Airfoil-2D-Panelmethod
- 使用Matlab语言编写的二维翼型Hess-smith面元法气动力计算程序-Using Matlab language Hess-smith airfoil aerodynamic surface element method calculation program
PANair
- 面元法程序,用于计算飞行器气动力、气动力矩系数。-panel code for aero calculation.
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)
面元法空气动力学例程-matlab
- 面元法计算升力阻力等,空气动力学小算例,模型基于三段模型,使用方法见标注
mianyuanfa
- 面元法求解面体表面压力分布,速度分布,输出数据文件,便于生成曲线图(The surface pressure distribution, velocity distribution and output data file are solved by the surface element method, which is convenient to generate graphs)
Mij_Hess_Smith
- matlab编程利用hess simth面元法(边界元法)计算球体及椭球体附加质量(Matlab programming uses hess_simth surface element method (boundary element method) to calculate the additional mass of spheres and ellipsoids)
TEST1
- 使用面元法计算机身的气动参数的matlab程序代码(Matlab code of aerodynamic parameters of computer body using panel method)