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frique SAR
- SAR成像仿真c++程序（机载条带模式、点阵目标、CS算法）-SAR imaging simulation c++ procedures（Airborne SAR with strip map mode,lattice targets,CS algorithm)
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
Flat-Plate-by-LBM
- 采用C语言，编写的基于格子Boltzmann算法计算平板绕流的程序代码。-Using C language, written in the flow around a program code based on lattice Boltzmann algorithm to calculate the plate.
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
avl3.31
- Drale编写的升力面模型，机翼表面被离散为涡格。与升力线模型相比，升力面模型更多的考虑了机翼的几何形状。-Lifting surface model Drale write the wing surface the discrete vortex lattice. Compared with the lifting line model, the lifting surface model consideration of the geometric shape of the wing.
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
D1Q3
- 格子Boltzmann方法一维入门程序 学习后可以改编为自己的程序-for Lattice Boltzmann Method study one dimensional entry procedures Can be adapted for your own program
UD
- 采用好格子点（GLP）的多变量多水平均匀实验设计法-Good lattice point method for uniform experimental design
les_lbm_cavity
- LES-LBM 大涡模拟-格子Boltzmann顶盖驱动方腔流动数值模拟-Large Eddy Simulation of Lattice Boltzmann lid driven cavity flow
nc
- 格子Boltzmann方腔自然对流数值模拟-Lattice Boltzmann simulation of natural convection Cavity flow
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. .
DLM
- 计算升力面非定常气动力的偶极子网格法MATLAB程序-Matlab functions to calculate unsteady aerodynamic pressures on a lifting surface using doublet lattice method.
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
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