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aiefoilconclution.rar
- 已知实验测得的翼型的压力分布和翼型数据，计算其升力系数和阻力阻力,Known experimental measured airfoil pressure distribution and airfoil data to calculate the lift coefficient and drag resistance
VLM
- 涡格法进行无人机的设计，升力系数，阻力系数，力矩系数等等，美过圣母大学的设计辅助软件-VLM
aa
- 目录 1 阻力系数和升力系数的计算 1 2 俯仰力矩系数的计算 1 3 法向力系数对攻角导数的计算 1 4 俯仰阻尼力矩系数的计算 2 5 俯仰阻尼力矩系数的推导 2-aerodynamic coefficient
source123
- 基于源板块法的matlab模拟无升力圆柱绕流程序。空气动力学中的一个实验-Matlab source plate method based on simulation of flow around a cylinder without lift procedure. Aerodynamics of an experiment
Fluent2D
- 飞机翼型的升力系数、阻力系数、压力中心等计算-Aircraft airfoil lift coefficient, drag coefficient, center of pressure computation
Airfoil
- 采用excel编写了翼型升力系数、阻力系数及力矩系数的360°扩展程序-Using excel to prepare the airfoil lift coefficient, drag coefficient and torque coefficient 360 extension
Wind-turbine-blades-design
- 本文利用MATLAB的遗传算法工具箱，对弦长和扭角沿风力机展向分布进行优化，得到设计工况下的最优叶片设计。目标函数是设计工况下基于动量叶素理论和Glauert等修正所得出的功率系数。在设计工况下得到的设计结果，其功率系数在一定的风速范围内都能保持一个较高的数值，同时其有效攻角分布大致都在所选翼型的升力与阻力系数的比值最大处，与理论相符合。其结果说明该优化实际的有效性。-In this paper, the use of MATLAB genetic algorithm toolbox, chor
VLM
- 用VLM编制了二维机翼的升力计算，与课本上的算例一致-VLM prepared by a two-dimensional airfoil lift calculations are consistent with the textbook examples
pablo
- 国外使用面元法计算翼型升力的matlab程序包-matlab program using panel method to solve the lift of the foil
Newton
- 1.采用数值积分法求解相对量运动微分方程组，计算燃料相对质量因数。(学过类似专业的应该明白算的是什么) 2.利用牛顿法计算某旋成体的升力、阻力、升阻比及俯仰力矩系数-Numerical integration method for solving differential equations of motion relative amount set calculating fuel relative quality factor. (Learned similar professional
ga_v1
- 用于翼型优化的遗传算法，比较简单，适用于一维情况，优化升力等- Genetic algorithms for optimization airfoil is relatively simple for the one-dimensional case, the optimization of the lift, etc.
Lift-fan
- 使用matlab语言计算升力风扇的总体参数，例如推力、效率、空气流量等参数-Matlab language calculated using the lift fan of the overall parameters, such as thrust, efficiency, air flow and other parameters
prophover
- 利用螺旋桨片条理论计算螺旋桨升力，功率，效率等参数。用于螺旋桨几何参数的优化-calculate the aerodynamic force of propellers
wogefa
- 进行无人机的设计，升力系数，阻力系数，力矩系数等等，美过圣母大学的设计辅助软件-Conduct UAV design lift coefficient, drag coefficient, torque coefficient, etc., over the United States and the University of Notre Dame assisted design software
m文件
- 选定翼型的叶片设计。针对一种翼型用MATLAB绘制了翼型界面图，计算了其升力系数，最终生成长度归一的叶片模型。(blade design for the chosen airfoil)