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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
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. Corresponding literature Time Domain M
Propellor
- 螺旋桨水动力性能计算的涡格法，求解涡量大小，表面压力预报 -Propeller hydrodynamic performance computing vortex lattice method for solving vorticity size, surface pressure forecast
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. .
Debug
- 计算机翼气动力的小程序方便使用，采用涡格法对机翼的升力进行计算，然后可以通过数据分析软件对结果进行拟合，从而得到机翼的升力线斜率。(The small program of the aerodynamic force of the computer is easy to use. The lift of the wing is calculated by the vortex lattice method, and then the results can be fitted by the da
avl3.36
- 适用于飞机概念设计，可以计算飞机的动静稳定性导数等。(Applicable to aircraft conceptual design, aircraft dynamic and static stability, derivatives and so on.)
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 design or in aeronautical educati
Vortex2D
- 输入naca四位数翼型，和环境参数，可以计算得到压力分布和升力系数(Pressure distribution and lift coefficient can be calculated by inputting NACA four-digit airfoil and environmental parameters.)