搜索资源列表
ST_Design
- 常用气动函数C++类代码,适用于航空工程计算-common aerodynamic function category C code that applies to aeronautical engineering calculation
03041505
- 对气动位置系统的嵌的工作原理、硬件构成和软件入式控制进行研究，介绍了其原理，并详细阐述一种气动阀门定位器智能控制系统设计-aerodynamic position on the embedded system's working principle, hardware and software-in control study , introduced his theory, and an elaborate pneumatic valve positioner Intelligent
thrust
- 飞行高度需在计算初设定，采用根据气动参数插值的方法计算最大平飞推力。-Altitude to be calculated at the beginning of setting, the use of aerodynamic parameters in accordance with the interpolation method the largest fly-ping thrust.
OpenDatcom_v1_1
- Datcom软件的GUI版，有界面 比普通的Dos操作要方便的多。用于计算气动数据！-Datcom the GUI version of the software, there are interface than the normal operation of the convenience of multi-Dos. Used to calculate the aerodynamic data!
1-5MW-a-wind-turbine
- 通过对试验结果的分析，研究获得了桨距角对风能利用系 数的影响规律，分析了不同叶尖速比下风轮转速急升和骤停现象与NH 系列翼型气动特性的关系- Through the analysis of test results, the obtained from the Angle of wind energy use OARS department The influence law of the number, analyzes the different rotor speed
F16aerodata
- F16气动数据，开环仿真，包括操作性及稳定性数据，前缘襟翼控制参数等。-F16 aerodynamic data, the open-loop simulation, including operational and reliability data, leading-edge flap control parameters.
Phi
- 计算入流角公式，自动绘制出入流角与叶尖速比之间的关系图，用于分析风机叶片的气动效率-To calculate the inflow angle formula, automatic drawing and out of the flow diagram of the relationship between the angle and tip speed ratio for the analysis of the aerodynamic efficiency of the fan blades
aircraft_trajectory_simulation
- 对某飞行器的全空域飞行弹道进行了仿真研究.建立了飞行器空间运动的数学模型，应用“牛顿插值多项式法”对气动力参数进行了辨识，用C语言编制了仿真程序，并给出了仿真结果及分析。-Of a vehicle-wide airspace simulation trajectory. Established the aircraft mathematical model of space motion, application, Newton interpolation polynomial method
Aero dynamic missile program
- 本程序的开发环境为MATLAB6.5版本，所编程序须在此环境下运行。由于气动模型的离散性，且采用了许多工程计算经验公式和实验数据，所以在编程时会比较繁杂，为了使程序读起来方便清晰，在编制程序时采用了如下的思路： 考虑到程序的一般结构，这里将气动计算系统分为三大模块：输入模块、气动计算模块以及结果输出模块。考虑到本系统的特殊性，又将输入模块划分为初始数据输入模块、导弹外形参数模块以及插值数据库模块，并采用M文件格式编制；气动计算模块则采用了子系统的结构形式，并用Simulink 模块编制；结
Missile_Guidance_Control_Systems
- The book presents a historical background of past and present guided missile systems and the evolution of modern weapons,discusses the generalized missile equations of motion, aerodynamic forces and coefficients, the important subject of the various
v1_turbine
- ANSYS的导弹尾翼建模及其气动分析， 是卡耐基梅隆大学网站上的一个ANSYS气动分析应用的例子，帮助理解ANSYS建模与分析，非常经典。-ANSYS modeling and aerodynamic missile fin analysis, is a Carnegie Mellon University on the website an example of application of ANSYS aerodynamic analysis to help understand the
aerodynamic
- 气动特性计算，包括全机焦点，升力系数，极曲线，动导数等-Calculation of aerodynamic characteristics, including the focus of the whole machine, lift coefficient, polar curves, such as dynamic derivatives
Aerodynamic-Performance-and-Stability-_thesis
- Aerodynamic Performance and Stability Simulation of Different Flying Wing Model Airplane Configurations thesis-Aerodynamic Performance and Stability Simulation of Different Flying Wing Model Airplane Configurations thesis
Aerodynamic-performance
- 提高风力机将风能转化为机械能的效率，根据我国西北地区的风频风能曲线，用最优设计攻角沿叶片轴线的非线性分布修正传统Wilson算法，优化设计大型水平轴风力机叶片的气动性 能．该优化设计利用Madab优化工具箱，优化速度干涉因子的迭代计算，提高计算效率；考虑多翼型和变攻角等因素对叶片外形优化的影响，从结构及加工工艺角度修正翼型．通过对1．2MW风力发电机组叶片外形的气动性能计算和优化设计，结果表明该优化设计的有效性和可行性，可为风力机叶片外形设计提供参考．-Improve wind turbin
Aerodynamic-Shape-Optimization-of-a-Re-entry-Caps
- Aerodynamic Shape Optimization of a Re-entry Capsule.pdf
Aerodynamic-Design-Analysis-of-the-HEXAFLY-INT.ra
- A good document regarding aerodynamic design of the hyper sonic vehicle
aerodynamic-calculation-of-propller
- 本代码为螺旋桨气动性能计算程序，可计算各种尺寸，螺距的螺旋桨在给定来流速度下的推力，功率和反扭矩气动特性，所采用的主要理论模型有螺旋桨动量叶素理论和牛顿迭代法。欢迎对该方面有兴趣的朋友共同研究，如有需要可联系。其中文件propmain为主程序。-The code for the propeller aerodynamic performance calculation program to calculate a variety of sizes, the main theoretical mo
Datcom
- 可用于计算机翼或全机低速飞行时的气动力，计算结果可以直接被matlab调用(Calculate the aerodynamic forces of a wing or whole aircraft at low speeds)
Aerodynamic Force
- 飞机气动力计算的程序，根据实际参数估算不同飞行状态下的气动力系数。(The aerodynamics calculation program, used to estimate aerodynamic coefficients under different flight conditions.)
Aerodynamic
- Aerodynamic performance of a wind-turbine rotor by means of OpenFOAM