搜索资源列表
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
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
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
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