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Description: 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
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Size: 4368 |
Author: hshnpu |
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Description: 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 Control System Design
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Size: 173140 |
Author: jake |
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Description: 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
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Size: 4096 |
Author: |
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Description: 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 Control System Design
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Size: 173056 |
Author: jake |
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Description: 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 of the node to adjust the wing grid, set up to flow speed, computer-wing aerodynamic. Finally by calculating the
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Size: 306176 |
Author: 窦怡彬 |
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Description: 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
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Size: 1024 |
Author: 丘重 |
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Description: 可压缩流体空气动力学分析软件，Fortran-Compressible fluid aerodynamic analysis software, Fortran
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Size: 4096 |
Author: 郭哲颖 |
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Description: 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 on the aerodynamic parameters identification, use of C language compiled simulation program, and to out the simulation results and analysis.
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Size: 107520 |
Author: 李恒 |
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Description: 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 types
of tactical guidance laws and/or techniques, weapon delivery systems and techniques,strategic
missiles and cruise missile theory and
design.
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Size: 3264512 |
Author: jbarragan |
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Description: 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 ANSYS modeling and analysis, very classic.
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Size: 319488 |
Author: jyll |
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Description: 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
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Size: 67584 |
Author: DingML |
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Description: 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
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Size: 2033664 |
Author: jes2012 |
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Description: 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 turbine wind energy into mechanical energy efficiency, according to the Northwest China wind frequency wind power curve, optimum design angle of attack along the blade axis of traditional non-linear distribution correction Wilson algorithm to optimize the design of the aerodynamic performance of the large-scale horizontal axis wind turbine blades . The Optimal Design Optimization Toolbox Madab optimized for speed interference factor iterative calculation to improve computational efficiency consider multi-airfoil and change the angle of attack and other factors on the blade shape optimization, airfoil from the structure and processing angle correction. By 1.2MW wind turbine blade shape aerodynamic performance calculation and optimization design, the results show that the effectiveness and feasibility of the optimized design can provide a reference for the wind turbine blade shape design.
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Size: 228352 |
Author: chentiange |
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Description: aerodynamic deisgn study of advanced multistage aixlal compressor
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Size: 6530048 |
Author: cai |
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Description: Aerodynamic Shape Optimization of a Re-entry Capsule.pdf
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Size: 169984 |
Author: behin |
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Description: A good document regarding aerodynamic design of the hyper sonic vehicle
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Size: 2607104 |
Author: MIRSOBANAHMED |
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Description: 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 model propeller pitch at a given flow velocity thrust, power and pneumatic anti-torque characteristics, used in propeller blade element momentum theory and Newton iteration law. Welcome friends who are interested in this aspect of the joint research, if necessary contact. Wherein the main program file propmain.
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Size: 4096 |
Author: 张凯 |
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Description: 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)
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Size: 30106624 |
Author: abao520
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Description: 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.)
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Size: 10240 |
Author: kkkkkjq
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Description: Aerodynamic performance of a wind-turbine rotor by means of OpenFOAM
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Size: 3164160 |
Author: eastleft |
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