搜索资源列表
proj3
- MIT--航空航天工程中的计算方法_有限元方法实例——涡轮叶片传热 MIT公开课程--航空航天工程中的计算方法 这门课程适用于在航空和航天工程中出现的计算方法的入门学习。其应用是从航空宇宙结构，空气动力学，动力学和控制，和航空宇宙系统选出的。其技术包括：常微分方程系统的数值积分；偏微分方程式的有限差分,有限体积, 和有限元的离散化；数值线性代数；本征值问题和带有约束的最优化。 -MIT- Aerospace Engineering in the finite elemen
Optimization-program
- MIT--航空航天工程中的计算方法_最优化方案 MIT公开课程--航空航天工程中的计算方法 这门课程适用于在航空和航天工程中出现的计算方法的入门学习。其应用是从航空宇宙结构，空气动力学，动力学和控制，和航空宇宙系统选出的。其技术包括：常微分方程系统的数值积分；偏微分方程式的有限差分,有限体积, 和有限元的离散化；数值线性代数；本征值问题和带有约束的最优化。 -MIT- Aerospace engineering calculations _ MIT open cou
gaochao
- 空气动力学高超声速 简单飞行器 气动力计算 -Aerodynamics of hypersonic aircraft aerodynamic calculations
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
missile-aerodynamics
- 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.
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
CFD
- This paper explain the Application of Computational Aerodynamics
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
NASA
- 几个飞机空气动力学方面的小软件，Java编写，包含代码，编辑即可执行。空气动力学方面、大气、引擎等-Several aircraft aerodynamics of small software, written in Java, contains the code, the editor can be executed. Aerodynamics, engine, air
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
DynamicDataSProc
- this zip is in ordeerer ot be read by the engineers responsible for car dynamics and aerodynamics of quadrotors
RocketModeler
- this zip when released for the applications of modeling of some severe body mechanical sudies inorder to be able to tackle some hard mechanical issues in the doamin of aerodynamics