搜索资源列表
Tomahawk2
- 通过对MatlAB 中Designing a Guidance System in MATLAB® and Simulink® 的导弹质量特性和气动特性的改变，并由原有的3DOF扩展为6DOF，仿真导弹的弹道特性、姿态特性和过载特性。 -In Matlab Designing a Guidance System in the MATLAB ® and Simulink ® missiles quality characteristics and aerodynamic characteris
gaochao
- 空气动力学高超声速 简单飞行器 气动力计算 -Aerodynamics of hypersonic aircraft aerodynamic calculations
missile-aerodynamics
- 导弹空气动力学，用于导弹计算流体力学和弹道仿真研究的参考书籍，非常系统和实用.-missile aerodynamic.This book is a good reference for CFD of missiles and Trajectory simulation.
Altair-structure-vibration
- Altair HyperWorks-结构振动和气动降噪方面的应用-Application of the Altair HyperWorks-structure vibration and aerodynamic noise
INTERP
- 提供一维与二维插值vb源程序，可实现不外插处理，非常适合气动力插值计算-Vb source of one-dimensional and two-dimensional interpolation can achieve nothing more than plug, ideal for the interpolation of the aerodynamic
S22_WT_Aerodynamic-Modeling
- Wind Turbine Aerodynamic modeling
Forces_Moments_Aero
- Aerodynamic Forces and Moments
windturb
- 采用遗传算法对风力机叶片气动外形进行优化设计，快速有效-Genetic algorithm to optimize the design of wind turbine blades aerodynamic shape, quickly and efficiently.
karmen_treffitzz-airfoil
- karman airfoil is very important in study of aircraft in particular and aerodynamic systems in general. study of karman airfoil in innovative idea in the field of aerodynamics.
wind-vehicle-bridge-coupling
- 采用数值模拟方法对风一车一桥耦合系统的车桥气动特性进行分析研究，模拟计算了不同工况下车 辆、桥梁的气动力系数．分析了车桥问相互的气动影响，研究结果表明．车桥耦合系统与桥梁和车辆各自单体 相比较．气动力系数差异较大．故建议进行风一车一桥系统耦合振动分析时。车桥气动力系数应考虑车桥问 的气动影响．-The numerical simulation method axle aerodynamic characteristics of the the wind car bridge coup
fletter
- 计算颤振，使用非定长气动力的方法进行计算，准确可靠-Calculated flutter, the use of non-fixed-length aerodynamic calculation, accurate and reliable
panair
- 亚声速超声速高阶空气动力学板块代码。所有线化理论板块方法中最可信和准确的。-High order aerodynamic panel code. The most versatile and accurate of all the linear theory panel codes. Subsonic/supersonic solutions with linear source strength variation and quadratic doublet strength variatio
MATLAB-for-trajectory
- matlab 实现三自由度无控弹道，程序中包含气动数据，适合飞行力学初学者学习-Matlab realize three degrees of freedom without controlled ballistic, contained in the aerodynamic data, suitable for beginners to learn flight mechanics
missile-rocket
- 一个关于导弹，火箭的程序，里面有阻力系数等气动参数。-A missile, rocket program, which drag coefficient and other aerodynamic parameters.
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
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
Aerodynamics_Volleyball
- A Parametric Analysis of the Aerodynamic Characteristics of Volleyballs.The main files are the VBPlotwKir (Volleyball Plot with Kirsten Data) and VBPlotwAVG (Volleyball Plot with Averaging). The other files are functions built for those files.
analysis-of-wind-turbine-blades
- 利用目前风力机叶片设计普遍采用的优化设计方法Wilson设计A-法，通过MATLAB编程，开发了小型叶片气动设计的应用程序，并利用该程序设计了一台3kW小型水平轴风力机叶片。采{用MATLAB和ANSYS共同建立了风力机叶片三维有限元参数模型，MATLAB编制的建模程序提高了{初期设计效率，缩短了ANSYS分析前处理时间。在此基础上进行了叶片固有振动特性计算，分析了叶《片的振动特性及其与结构参数之间的关系，分析方法和结果对风电叶片的结构设计和动力分析有一定；的参考价值。-Advantage of
Source
- AeroDyn风力机叶片空气动力学计算程序的内核，来自美国可再生能源实验室-AeroDyn is a set of aerodynamic loads code for wind turbine blades, which is developed by NREL
nseg
- NSEG是美国兰利研究中心推出的飞行器起飞、爬升、巡航、加速、下降、减速和着陆等各个过程分析软件。-NSEG was developed to perform rapid aircraft mission analyses. It is based upon the use of approximate equations of motion whose form varies with the type of flight segment. Flight segments consid