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wogefa
- 涡格法是空气动力学中的常用方法之一，这个程序可以通过自己设置机翼的节点来调整机翼的网格，设置来流速度，计算机翼的气动力。最后通过计算《空气动力学》教程中的一个涡格法算例验证了程序的正确性
涡格法计算算例
- 涡格法计算机翼涡强算例
涡格法计算算例2
- 涡格法计算机翼涡强，并且就几个不同参数进行比较分析
wogefa
- 涡格法是空气动力学中的常用方法之一，这个程序可以通过自己设置机翼的节点来调整机翼的网格，设置来流速度，计算机翼的气动力。最后通过计算《空气动力学》教程中的一个涡格法算例验证了程序的正确性-Vortex lattice method is commonly used in aerodynamics one of the methods, this procedure can be set up through their own wing
CharacteristicsAnalysisofLimited-Aspect-RatioWingB
- 涡格法计算有限展弦比机翼升力的程序，提供给研究机翼或螺旋桨的朋友-Characteristics Analysis of Limited-Aspect-Ratio Wing By Vortex-Lattice Method
HVLL
- 经典螺旋桨设计程序 采用精确度较高的涡格法-propeller design Vortex Lattice method
VLM
- 涡格法进行无人机的设计，升力系数，阻力系数，力矩系数等等，美过圣母大学的设计辅助软件-VLM
luoxuanjiang
- 涡格法计算机翼涡强，现目前主要写出了计算涡强部分，升阻力后续传上-Vortex lattice method the computer wing vortex strength
wogefajisuan
- 涡格法计算机翼的涡强，对不同剖面形状，拱度等进行了比较分析。-Vortex lattice method the computer wing of the vortex is strong, the shape of different profiles, such as camber, a comparative analysis.
wogefasuanli
- 涡格法计算机翼的涡强，对不同剖面形状，拱度等进行了比较分析。并且与书籍上对比-Vortex lattice method the computer wing of the vortex is strong, the shape of different profiles, such as camber, a comparative analysis.
Vortex-lattice-FORTRAN-planforms
- fortran语言的涡格法估算亚音速流场特性的程序文档和方法-vortex lattice method estimates fortran language subsonic flow field characteristics of program documentation and methods
flapping
- 使用非定常涡格法(UVLM)计算一种简单扑翼机的升力。对应文献Time Domain Modeling of Unsteady Aerodynamic Forces on a Flapping Airfoil -Eric Durand（MIT Master thesis）-Unsteady vortex lattice method (UVLM) a simple flapping wing machine lift. Correspo
wogewoge0
- 涡格法求解翼型的气动力，包括阻力 升力 法向力-Vortex lattice method for solving the the aerodynamic airfoil, including resistance lift normal force
T135_export
- 涡格法计算现行气动力的matlab代码，用于飞机机翼概念设计阶段的气动力评估-Tornado is a Vortex Lattice Method for linear aerodynamic wing design applications in conceptual aircraft design or in aeronautical education
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)
涡格法代码
- 涡格法计算机翼的表面的升力和升力系数，采用高斯迭代求解(The lift and lift coefficients on the surface of the computer wings of the vortex lattice are solved by Gauss iteration)
AB
- 非线性涡格法公式编程，用matlab打开(Nonlinear vortex lattice formula programming, open with MATLAB)
涡格法计算升力
- 利用涡格法计算对称机翼的升力，压心和焦点(Calculation of lift force, center of pressure and focus of symmetrical wing by vortex lattice method)
涡格法
- 采用涡格法估算低速飞机纵向气动特性，包括升力系数、阻力系数及俯仰力矩系数！(It's a great matlab program)
T135_export
- Tornado，改进涡格法的MATLAB程序。自带NACA翼型库，是比较成熟的程序。简单好用。(This is the new webpage for Tornado Vortex Lattice method. Tornado is a Vortex Lattice Method for linear aerodynamic wing design applications in conceptual aircraft des