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wuyeguanli
- 物业管理系统,VB做的,小试牛刀,不吝赐教-Property Management System, VB do small test chopper, the wing
CharacteristicsAnalysisofLimited-Aspect-RatioWingB
- 涡格法计算有限展弦比机翼升力的程序，提供给研究机翼或螺旋桨的朋友-Characteristics Analysis of Limited-Aspect-Ratio Wing By Vortex-Lattice Method
danyijianmo
- ANSYS弹翼建模方法及其源代码，详细描述了ANSYS建模过程，针对给定导弹参数建立了导弹弹翼模型并对其进行应力应变分析。-ANSYS wing modeling method and its source code, a detailed descr iption of the ANSYS modeling process, parameters for a given missile missile wing was established models and analysis of st
feijijiyiwanjianniujisuan
- 题目所给飞机机翼受的是平均载荷，所以要计算每一站点上的剪力，弯矩和扭矩，就要先算出其所在平面的面积和其合力作用线到某一座标轴的距离，及集中载荷作用线到中心线的距离。带载荷等于面积乘以平均载荷，某一站点剪力等于此站点之前所有带载荷之和。弯矩等于剪力乘以合力作用线到其对应坐标轴的距离。扭矩等于剪力乘以集中载荷作用线到中心线的距离。所得结果与笔算结果基本吻合。程序具有一定的通用性。-Subject to the aircraft wing by the average load is, so each
koron
- 科荣软件，提供企业信息化解决方案！帮忙企业腾飞。-Section Wing Software provides business information solutions! Help businesses take off.
vertex
- 该程序可用于计算无后缘后掠角的平板梯形翼在小攻角时升力与升力系数-This program can be used to calculate the plate without posterior trapezoidal wing sweep angle of attack in the small lift and lift coefficient
GFOSUB_N
- 基于麦克马公司设计的折叠翼飞行器的折叠翼气动力加载程序-Designed based on McMahon folding wing aircraft folding wing aerodynamic loader
openprop.tar
- 升力线模型计算代码，将机翼表征为一个沿展向变化的涡线，通过尾涡计算诱导速度，实现计算的封闭。-Lifting line model code, the characterization of the wing along the exhibition to the change of the vortex line, trailing vortex induced velocity calculated closed.
Liftind-line
- Fortran版本的升力线模型源代码，目前只能计算平板机翼，尾涡模型采用的刚性螺旋尾涡。-Fortran version of the the lift line model source code can only calculate the flat-panel wing the rigid spiral trailing vortex wake model used.
avl3.31
- Drale编写的升力面模型，机翼表面被离散为涡格。与升力线模型相比，升力面模型更多的考虑了机翼的几何形状。-Lifting surface model Drale write the wing surface the discrete vortex lattice. Compared with the lifting line model, the lifting surface model consideration of the geometric shape of the wing.
flapping
- 使用非定常涡格法(UVLM)计算一种简单扑翼机的升力。对应文献Time Domain Modeling of Unsteady Aerodynamic Forces on a Flapping Airfoil -Eric Durand（MIT Master thesis）-Unsteady vortex lattice method (UVLM) a simple flapping wing machine lift. Corresponding literature Time Domain M
Flight_control
- 简易固定翼飞机纵向和侧向飞行控制系统设计仿真，dat0-dat9分别为9个不同参数飞机的相关参数文件-Simple fixed-wing aircraft longitudinal and lateral flight control system design and simulation, dat0-dat9 were nine different parameters related to aircraft parameter file
flutter
- 采用片条理论进行机翼的颤振分析，匹配点和非匹配点分析-Carried out using strip theory wing flutter analysis, matching and non-matching point analysis points
Qwin
- 组合翼面涡法Fortran核心程序，求解机翼的速度和压力分布-Combination of airfoil core eddy France Fortran program to solve the wing velocity and pressure distribution
2d-airfoil-release2.0
- 2d-airfoil-release2.0，解2维机翼的面元法，运行时放在英文目录下-2d-airfoil-release2.0, solutions of two-dimensional wing panel method, the runtime directory in English
dynamic-model-of-fixed-aircraft
- 基于simulink环境的areospace模块的固定翼飞行器动力学建模与控制-Dynamic modeling and control of fixed-wing aircraft based on simulink environment areospace module
wangge1
- 使用涡格法计算任意翼面的升力、阻力、俯仰力矩系数-CALCULATING wing vortex lattice method of using lift, drag, pitching moment coefficients. .
APM-fixed-wing-set-complete-manual
- APM固定翼飞控设置完整手册，为不会玩apm的玩家开发板子提供基础支持-APM fixed wing set complete manual
7759-AHU4
- wING DIAGRAMS FOR ahu
butterflylight_latest.tar
- The Butterfly Light is an open source, modular FPGA development board. It is comprised of the USB Cocoon and the Spartan 3E Cocoon which paired together create the Butterfly Light FPGA development board. The Butterfly Light is best suited for develop