搜索资源列表
DATCOM
- 实现导弹的气动参数计算，各种气动参数的计算。-Achieve missile aerodynamic parameter calculation, calculation of various aerodynamic parameters.
Load_V2.0
- 此程序根据王专利撰写的《翼面结构有限元模型节点气动载荷计算》编写 需要的前期准备文件：case01.txt---已知不同工况下各个载荷点力的文件 Force_Site.txt---已知各个载荷点的坐标 Node_Site.txt----有限元节点坐标 输出文件 Nodal_Force_01.txt----存放每个有限元节点计算后分得的力，第一列为节点编号，第二列为节点力大小-This process patent under the king wrote &quo
123
- 液压气动设备计算 工作压力缸筒内径安全系数抗压指数-Hydraulic and pneumatic equipment working pressure cylinder diameter calculated safety factor of compression index
hypersonic-modified-model
- 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
elastic
- 计算静气动弹性的程序，主要功能包括计算q，和alpha 静稳定性以及表面诱导阻力-Static aeroelastic calculation procedures, the main features include computing q, and alpha-induced static stability and surface resistance
weightpositioncalculation
- 通过移动机翼，尾翼，起落架和油箱的位置来使气动中心和重心重合。-By movingwings, tail, landing gearand fuel tankpositionto makethe aerodynamic centerand center of gravitycoincide.
noncontrol-ballistic-simulation
- Matlab编写的纵向平面内无控弹道仿真程序，（内含气动数据），采用线性插值与4阶龙格库塔法解算常微分方程组-The longitudinal plane Matlab prepared uncontrolled trajectory simulation program (includes aerodynamic data), using linear interpolation with four first-order Runge-Kutta method ODE solver
Multi_point
- 此段程序详细演示了如何将飞机机翼所受的气动载荷等效的加载到有限元节点上的过程，采用方法是“多点排法”-This program aims adding the aerodynamic forces onto the finite element nodes. The method which it used is the Multi-point method
DHJ_QK
- 气动电焊机主控制程序，具有气缸控制，可控硅移相触发控制功能，实现电焊机的自动碰焊功能-Pneumatic welding machine main control program, with cylinder control, SCR phase trigger control functions, to achieve automatic welding machine Welding function
Trajectory-simulation-program
- 包含了铅垂平面内弹道仿真的matlab程序（不带有气动参数，需要自己给定），含有差值，仿真的整个过程。导弹飞行动力学材料。-Contains the vertical plane trajectory simulation matlab program (not with the pneumatic parameter, needs its own given), contains the difference, the whole process simulation. Missile fli
find-from-excel
- 查询EXCEL中翼型的空气动力系数值,如气动力矩，升力系数，阻力系数等-find date excel
OpenProp
- 螺旋桨气动性能估算程序，计算拉力，扭矩，功率，精度较高-Propeller aerodynamic performance estimation procedure
PANair
- 面元法程序，用于计算飞行器气动力、气动力矩系数。-panel code for aero calculation.
airfoilprep
- 一种用于风力机设计和性能校核的翼型气动数据预处理，包括panel插值，全周插值，3D修正等。使用python语言 -Airfoil data preprocessing for wind turbine design and performance verification using python language
Four-rotor-Simulator
- 四旋翼飞行仿真计算,对旋翼进行气动仿真计算，以及控制设计-Four-rotor flight simulation
datcomexec
- 气动计算软件DATCOM，美国空军用，飞行器设计初期气动参数估算很好的软件。-Aerodynamic calculation software DATCOM, the United States Air force used, the initial design of aircraft aerodynamic parameter estimation is very good software.
RehaRobot-0529
- 基于vc++6.0的上肢外骨骼康复机器人的控制系统。该控制系统通过采集卡获得机器人的关节角数据，运用非线性PID实时运算得到气动肌肉的气压给定量，并通过AD 输出实现规划的被动康复运动。-Vc++ 6.0 control system exoskeleton upper limb rehabilitation robot based on. The control system is obtained by the robot joint angle data acquisition card,
FAST_v8.10.00a-bjj.tar
- 这是一个风力机的气动软件，可以算是一个新新之秀，国内现在也有很多个人和公司在使用，的确是替代blade的一个优秀的开源fortran软件-A software used to perform simulation with wind turbine
aeroelasticity
- 计算气动弹性力学中的发散动压，发散速度，载荷重新分布等问题-Calculation aeroelasticity divergence dynamic pressure, diverging speed, load redistribution and other issues
Boltzmann-acoustic-VC
- 不可压缩空腔流动的气动声学模拟，采用格子-玻尔兹曼方法，C语言源代码-Aeroacoustics simulate incompressible flow cavity, using Lattice- Boltzmann method, C language source code