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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
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
wogefa
- 涡格法是空气动力学中的常用方法之一，这个程序可以通过自己设置机翼的节点来调整机翼的网格，设置来流速度，计算机翼的气动力。最后通过计算《空气动力学》教程中的一个涡格法算例验证了程序的正确性-Vortex lattice method is commonly used in aerodynamics one of the methods, this procedure can be set up through their own wing
boundary
- 计算气动力边界条件，非守恒无激波跨声速情况下使用-Calculation of the aerodynamic boundary conditions, non-conservation of transonic shock-free use
CompAeroSCode
- 可压缩流体空气动力学分析软件，Fortran-Compressible fluid aerodynamic analysis software, Fortran
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 in
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.
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 imp
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 a
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 thes
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
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
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