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996503102
- 空气动力学中壁面层流的计算文件，可以计算任一点的压强和速度等物理量，适用于薄壁-Wall laminar flow aerodynamics calculation file can be calculated at any point of the physical quantities such as pressure and speed, suitable for thin-walled
mpxfoil_0.1.tar
- Using XFOIL based on Lifting Surface Theory to Achieve 3-D Aerodynamics
shockwave
- A program to demonstrate shock wave intersection in aerodynamics.This programme will calculate two shock wave angle form the angle of flow derection changing, and then give the result of the intersection.at last there will out put a tecplot file to g
dgfem
- 本文件夹中的文件是用间断Galerkin方法求解守恒律方程、空气动力学的Euler方程和浅水波方程-The files in this folder is discontinuous Galerkin method for solving the equation of conservation laws, the aerodynamics of the Euler equations and shallow water wave equation
Parasitic-coefficient
- Parasitic drag (also called skin friction drag) is drag caused by moving a solid object through a fluid medium (in the case of aerodynamics, more specifically, a gaseous medium). Parasitic drag is made up of many components, the most prominent being
Basic-Rocketry-Aerodynamics
- Basic rockets Equations
karmen_treffitzz-airfoil
- karman airfoil is very important in study of aircraft in particular and aerodynamic systems in general. study of karman airfoil in innovative idea in the field of aerodynamics.
Wagner-approximate
- 非定常气动力Wagner问题求解，突然迎角阶跃非定常气动力-Wagner UNsteady aerodynamics
w12sc3
- W12SC3是美国基于USSAERO程序的超声速机翼设计及分析代码，可用于机翼的整个设计、分析及优化过程。-W12SC3- Supersonic wing design and analysis using source and vortex panel singularity distributions, based on the USSAERO program by Woodward. W12SC3 combines source and vortex panel singulari
vlmd
- 计算低速气动力的涡格法程序，来自NASA，可信度高-This is a vortex lattice aerodynamic program from the low speed aerodynamics group at NASA Langley
motecalor
- 蒙特·卡罗方法（Monte Carlo method），也称统计模拟方法，是二十世纪四十年代中期由于科学技术的发展和电子计算机的发明，而被提出的一种以概率统计理论为指导的一类非常重要的数值计算方法。是指使用随机数（或更常见的伪随机数）来解决很多计算问题的方法。与它对应的是确定性算法。蒙特·卡罗方法在金融工程学，宏观经济学，计算物理学（如粒子输运计算、量子热力学计算、空气动力学计算）等领域应用广泛。-Monte Carlo (Monte Carlo method), also known as s
FASER-Test-158-Forced-Oscillation-Reduced-Data.zi
- matlab program to learn how to control uav with its aerodynamics for helping for special case faser uav
AeroSim
- 提供一整套六自由飞行器simulink模块，包括非线性运动方程、空气动力学、执行机构、传感器等-The AeroSim blockset provides a complete set of tools for developing nonlinear 6-degree-of-freedom aircraft dynamic models. The Simulink blocks include the nonlinear equations of motion, linear aero
qidongli
- Grossman气动力，可用于获取Volterra级数一阶核的特征系统辨识的输入输出仿真。-Grossman aerodynamics can be used to obtain a first-order Volterra series features core simulation input and output system identification.
Other-Project
- Aerospace engineering codes for low speed aerodynamics
VLMpc
- Vortex lattice analysis and design: VLMpc-John Lamar s two surface vortex lattice program, developed at NASA Langley. The program treats two lifting surfaces using up to 200 panels. Vortex flows are estimated using the leading edge suction analogy. T
CFD-FDV
- 美国T.J. chung教授所著《Computational Fluid Dynamics》配套程序，主要用于高速空气动力学计算。-The source code of Computational Fluid Dynamics by T.J. Chung, mainly used for aerodynamics.
function
- 空气动力学中常用压力、密度、温度、激波角等公示的调用函数程序，使用matlab编写。-Aerodynamics commonly used pressure, density, temperature, shock angle publicity program calls the function using matlab prepared.
four-rotor-aircraft
- 关于飞行器的研究，建立四旋翼飞行器基于刚体的初步力学模型，及参数测量，研究多旋翼飞行器的空气动力学特性。基于模型的控制算法。-Research on the aircraft, the establishment of four-rotor aircraft based on preliminary mechanical model of a rigid body, and parameter measurement, Multi-rotor aerodynamics. Model-based
mK
- 蒙克卡罗 蒙特·卡罗方法（Monte Carlo method），也称统计模拟方法，是二十世纪四十年代中期由于科学技术的发展和电子计算机的发明，而被提出的一种以概率统计理论为指导的一类非常重要的数值计算方法。是指使用随机数（或更常见的伪随机数）来解决很多计算问题的方法。与它对应的是确定性算法。蒙特·卡罗方法在金融工程学，宏观经济学，计算物理学（如粒子输运计算、量子热力学计算、空气动力学计算）等领域应用广泛。-蒙克卡罗蒙 Carlo method (Monte Carlo method), als