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  1. 03041505

    0下载:
  2. 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
  3. 所属分类:软件工程

    • 发布日期:2008-10-13
    • 文件大小:173140
    • 提供者:jake
  1. 1-5MW-a-wind-turbine

    1下载:
  2. 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
  3. 所属分类:软件工程

    • 发布日期:2017-05-18
    • 文件大小:405116
    • 提供者:马忠鑫
  1. aircraft_trajectory_simulation

    4下载:
  2. 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
  3. 所属分类:software engineering

    • 发布日期:2014-12-29
    • 文件大小:108144
    • 提供者:李恒
  1. Missile_Guidance_Control_Systems

    0下载:
  2. 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
  3. 所属分类:Project Design

    • 发布日期:2017-05-13
    • 文件大小:3264947
    • 提供者:jbarragan
  1. Interference

    0下载:
  2. 介绍了子母弹气动干扰风洞实验新方案的特点及实验装置的构成。利用该方案进行了布撒 器 —子弹气动干扰风洞实验。-Describes the shrapnel Aerodynamic wind tunnel tests of the new program features and the composition of experimental devices. Using the program was Dispenser- Bullet aerodynamic interference wi
  3. 所属分类:Development Research

    • 发布日期:2017-03-27
    • 文件大小:173746
    • 提供者:王顺红
  1. SpaceFlightDynamics

    0下载:
  2. The ballistic category of atmospheric vehicles includes missiles, launch ve- hicles, and entry capsules. Some missiles and launch vehicles incorporate fi ns as aerodynamic stabilizing and control surfaces. The spacecraft are also catego-
  3. 所属分类:Development Research

    • 发布日期:2017-05-24
    • 文件大小:7983247
    • 提供者:kalaiarasan.R
  1. missile-aerodynamics

    2下载:
  2. 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.
  3. 所属分类:Development Research

    • 发布日期:2017-05-25
    • 文件大小:8304742
    • 提供者:Neil
  1. S22_WT_Aerodynamic-Modeling

    0下载:
  2. Wind Turbine Aerodynamic modeling
  3. 所属分类:Development Research

    • 发布日期:2017-04-24
    • 文件大小:59708
    • 提供者:hamid
  1. wind-vehicle-bridge-coupling

    1下载:
  2. 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
  3. 所属分类:File Formats

    • 发布日期:2017-11-24
    • 文件大小:439995
    • 提供者:dddd
  1. Aerodynamic-Performance-and-Stability-_thesis

    0下载:
  2. 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
  3. 所属分类:Development Research

    • 发布日期:2017-11-16
    • 文件大小:2033664
    • 提供者:jes2012
  1. hypersonic-modified-model

    1下载:
  2. 高超声速飞行器再入过程改进气动系数模型,建模的可以参考学习-Modified aerodynamic coefficient models of hypersonic vehicle in reentry phase
  3. 所属分类:File Formats

    • 发布日期:2017-04-09
    • 文件大小:367208
    • 提供者:韩苏
  1. Aerodynamic-Shape-Optimization-of-a-Re-entry-Caps

    0下载:
  2. Aerodynamic Shape Optimization of a Re-entry Capsule.pdf
  3. 所属分类:Project Design

    • 发布日期:2017-04-24
    • 文件大小:169967
    • 提供者:behin
  1. datcom

    1下载:
  2. datcom software aerodynamic predection aiaa datcom software aerodynamic predection aiaa datcom software aerodynamic predection aiaa -datcom software aerodynamic predection aiaa datcom software aerodynamic predection aiaa datcom softwar
  3. 所属分类:software engineering

    • 发布日期:2015-05-13
    • 文件大小:636928
    • 提供者:rfgjcrtthjdhj
  1. Aerodynamic-Design-Analysis-of-the-HEXAFLY-INT.ra

    0下载:
  2. A good document regarding aerodynamic design of the hyper sonic vehicle
  3. 所属分类:Project Design

    • 发布日期:2017-05-13
    • 文件大小:2607078
    • 提供者:MIRSOBANAHMED
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