搜索资源列表
F16Sim--University-of-Minnesota-2003
- F16战斗的飞行仿真程序，可以根据机翼的运动变化计算出飞机的飞行轨迹。-F16 combat flight simulation program can calculate the flight path of the aircraft under the wing of the movement changes.
openprop.tar
- 升力线模型计算代码，将机翼表征为一个沿展向变化的涡线，通过尾涡计算诱导速度，实现计算的封闭。-Lifting line model code, the characterization of the wing along the exhibition to the change of the vortex line, trailing vortex induced velocity calculated closed.
Liftind-line
- Fortran版本的升力线模型源代码，目前只能计算平板机翼，尾涡模型采用的刚性螺旋尾涡。-Fortran version of the the lift line model source code can only calculate the flat-panel wing the rigid spiral trailing vortex wake model used.
FULTTER-COM
- 计算二元机翼的颤振速度，包含一个经过处理的时间延迟环节-Calculated airfoil flutter speed, contains a treated time delay link
src
- 计算二维翼型升阻力系数及翼型设计，广泛的用于风机翼型以及风力机等翼型设计-Calculation of two-dimensional airfoil lift and drag coefficients and airfoil design
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.
WING-MATLAB-CODE
- 详细介绍了飞机翼型的分析过程，具有很好的实际应用效果-Aircraft airfoil analysis process, and has a very good application effect
Matlab-Optimization-tools
- 基于Matlab软件中的优化算法和优化工具，针对风力机翼型通用型线集成表达式建立了优化数学模型。以风力机翼型的最大升阻比为优化设计目标函数，翼型形状控制方程的系数为设计变量，翼型的厚度和弯度为约束条件，设 计得到了相对厚度为18％的风力机翼型，并对其性能进行了计算分析。研究结果拓宽了风力机叶片翼型的设计思路和设计方法。-Based the Matlab software optimization algorithm and optimization tools for the integra
w12sc3
- W12SC3是美国基于USSAERO程序的超声速机翼设计及分析代码，可用于机翼的整个设计、分析及优化过程。-W12SC3- Supersonic wing design and analysis using source and vortex panel singularity distributions, based on the USSAERO program by Woodward. W12SC3 combines source and vortex panel singulari
Flutter
- 这个程序演示了如何应用耦合结构空气动力问题，通过Matlab编程，分析了飞行器机翼颤振等问题。-This model demonstrates how to implement a coupled structural-aerodynamic problem. The wing, otherwise rigid, is allowed to pitch and plunge. The motion of the wing is defined using SimMechanics bloc
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
flutter
- 采用片条理论进行机翼的颤振分析，匹配点和非匹配点分析-Carried out using strip theory wing flutter analysis, matching and non-matching point analysis points
weightpositioncalculation
- 通过移动机翼，尾翼，起落架和油箱的位置来使气动中心和重心重合。-By movingwings, tail, landing gearand fuel tankpositionto makethe aerodynamic centerand center of gravitycoincide.
c_grid
- 机翼、翼型 C 网格生成程序 fortran code-fotran code ，C grid fortran fur airfoil and win
VLM
- 用VLM编制了二维机翼的升力计算，与课本上的算例一致-VLM prepared by a two-dimensional airfoil lift calculations are consistent with the textbook examples
EGAB
- 运用MATLAB建立飞机模型，机翼 机身的源代码-use MATLAB creat a airplane model
shape-context
- 形状上下文：机翼跟踪，高清PDF文档，5页-Shape Context: wing papers in English from the original track tangent, HD, pdf format,
Multi_point
- 此段程序详细演示了如何将飞机机翼所受的气动载荷等效的加载到有限元节点上的过程，采用方法是“多点排法”-This program aims adding the aerodynamic forces onto the finite element nodes. The method which it used is the Multi-point method
AirfoilGeometry
- 机翼编程，有助于对机翼设计，网格划分带来帮助-Wing Programming
optimization-for-wind-turbine
- 基于动量叶素理论的风力机翼型优化，程序为MATLAB编写-Optimization of wind turbine airfoil