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modifycircuit
- 公交线路随点随改 ---请用鼠标拖动图标的方法修改线路-Please use the mouse to drag an icon way modify the circuit
cxcy
- 黑鹰桨叶升力/阻力/力矩系数随迎角变化数据模型-The paddle lift/drag/moment coefficient different angles of attack data
Fluent-history-result-postprocess
- Fluent软件通常用于航空航天领域，本程序可以实现对Fluent计算结果的自动提取，并且按照来流迎角对升阻力、力矩系数排序，最后生成结果文件-Fluent software is typically used for aerospace applications, this program can achieve automatic extraction Fluent calculation results, and in accordance to the flow angle of att
matlab-xfoil
- 通过matlab调用xfoil程序，对翼型升阻力力矩进行计算，并将计算结果生成结果文件，程序中对三种翼型进行了计算，用户可根据需要删减或复制程序的相同部分即可-Xfoil by calling the same part of matlab procedures, the airfoil lift and drag torque is calculated, and the calculated results file is generated, the program for the thr
wangge1
- 使用涡格法计算任意翼面的升力、阻力、俯仰力矩系数-CALCULATING wing vortex lattice method of using lift, drag, pitching moment coefficients. .
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.