搜索资源列表
vpm
- 二维涡流位置及流场分布计算程序，Vortex Panel Method
pablo
- Vortex Panel Method
MiniDrawPad
- 本程序通过调用JAVA提供的BasicStroke；Button； Color Container Graphics Panel ButtonGroup JFrame JComboBox；JCheckBox；JMenu；JMenuItem；ImageIcon；JPanel UIManager等基本类进行了简单的界面设计。 程序运用了JAVA中类的继承特性实现了对父类方法的调用，运用了ButtonHandler类用来侦听基本按钮的操作；运用ButtonHandler1类侦听颜色选择，画笔粗细设
A-practical-method-for-flat-panel-high-precision-c
- 一种实用的平板高精度摄像机标定方法A practical method for flat-panel high-precision camera calibration-A practical method for flat-panel high-precision camera calibration
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-viewPort
- 使用最先进的extjs4.0技术，结合asp.net方法，生成的viewport，方便搭建框架-Use most advanced extjs4.0 of technology, combined with the asp.net method to generate the viewport, and convenient to build the framework
0_25059600_1353476662-(1)
- source-panel Method. it is very strong
panel-(1)
- A hess and smith panel method code for aerofoil analysis
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
JTableDemo1
- 窗体的实现,面板的方法,表格的使用,以及一些方法-Form of implementation, panel method, use of forms, as well as some methods
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
panelmethod
- source panel method matlab code for cylinder
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
CODE
- panel method for aerodynamics usage
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.
pablo
- Pablo is a pedagogical low-speed airfoil analysis program written in MATLAB. It uses a one way coupled inviscid + boundary layer model. The inviscid flow is solved using a Panel Method [1]. Three different kinds of singularity distributions can
MATLAB
- a panel method for airfoil