搜索资源列表
helimodel
- 完备的无人直升机数学建模指导方案，包括：主旋翼、尾桨和整体空气动力学说明-helicopter modelling
F16aerodata
- F16气动数据，开环仿真，包括操作性及稳定性数据，前缘襟翼控制参数等。-F16 aerodynamic data, the open-loop simulation, including operational and reliability data, leading-edge flap control parameters.
aerolab1.3
- 一款十分实用的可绘制导弹气动外形的工作软件，画图迅速，精确，十分难得！-A wonderful software for drawing many missile configurations!
flightdesignprogramusingmatlab
- 飞机设计的相关程序,全机总体参数计算程序 ,全机气动曲线计算程序 ,机翼载荷分布计算程序,巡航状态纵向动稳定性计算程序 ,横航向稳定性计算程序,平飞速度范围计算程序,螺旋桨特性计算程序 -program about flight design including most of problems in flight design
Phi
- 计算入流角公式，自动绘制出入流角与叶尖速比之间的关系图，用于分析风机叶片的气动效率-To calculate the inflow angle formula, automatic drawing and out of the flow diagram of the relationship between the angle and tip speed ratio for the analysis of the aerodynamic efficiency of the fan blades
aircraft_trajectory_simulation
- 对某飞行器的全空域飞行弹道进行了仿真研究.建立了飞行器空间运动的数学模型，应用“牛顿插值多项式法”对气动力参数进行了辨识，用C语言编制了仿真程序，并给出了仿真结果及分析。-Of a vehicle-wide airspace simulation trajectory. Established the aircraft mathematical model of space motion, application, Newton interpolation polynomial method
QIDONGGUI
- 基于VB的气动规零件公差测量系统，一个生产流水线上的零件测量软件。-VB-based regulatory components of the pneumatic measuring system tolerances, a production line on the measurement of software components.
takeoff
- 飞机起飞性能计算，确定飞机的起飞性能，包括滑跑距离、起飞距离、起飞时间、离地速度，气动修正考虑了收放起落架、襟翼的影响，但未考虑地面效应.-Aircraft take-off performance calculations to determine the aircraft s takeoff performance, including the roll distance, takeoff distance, takeoff time, off speed, the amendment ta
QQ
- 主要实现接受和发送信息的功能。气动并属兔对方IP后单击连接按钮，来实现，能很好说明。NET在中Socket编程技术 -Mainly to receive and send messages to achieve functions. Pneumatic and other IP is a rabbit and click connect button, to achieve, can be a very good note. NET programming in Socket
library
- 超级符号库,提供电气符号,工艺表格图样,机构运动符号,夹具库,液压气动符号库等等.AUTOCAD格式.-Super-symbol library, to provide electrical symbols, forms design process, the movement symbols, fixture library, hydraulic pneumatic symbol library and so on. AUTOCAD format.
kqdlx
- as轿车空气动力学演示-as car aerodynamics demo! ! ! ! ! ! ! ! ! ! ! ! ! ! ! ! !
F15E
- F15E的3D图，能够直观反映该机型的外形特征及翼型布局，对研究该机型的气动外形及辐射特征有一定的参考价值-F15E, 3D map, be able to intuitively reflect the characteristics and airfoil shape model layout of the study of the aircraft' s aerodynamic shape and radiation characteristics of a certain refe
SystemParameterIdentification
- 用广义最小二乘法辨识气动实验系统的参数，并采用最终误差预报估计模型阶次-Generalized Least Squares Identification of aerodynamic parameters of experimental system, using the final prediction error of the estimated model order
Application
- 对弹丸飞行稳定性进行了分析,文中提出利用M GAERO 气动软件计算弹丸的气动力参数,以减少采 用经验公式估算气动力系数和压心位置等参数带来的误差,可为弹丸飞行稳定性分析和总体参数设计提供 参考依据。-For projectile flight stability analysis, this paper proposes the use of software to calculate projectile M GAERO aerodynamic aerodynamic paramet
Aerodynam
- 运用流体力学数值计算软件对有头部攻角的弹丸气动性能进行了数值计算, 分析了有头部攻角弹 丸周围流场和作用在弹丸表面的空气动力. -The use of numerical fluid dynamics software to have the head of the projectile angle of attack aerodynamic performance of the numerical calculation, analysis of a head attack angle s
EFFECTS
- 本文应用重叠网格技术对子母弹分离过程中多体无粘超声速流动进行了数值仿真。采用 NND 格式,通过求解Euler 方程,给出了母弹附近的子弹气动干扰特性。-In this paper, separation of overlapping grid of cluster bombs during the multi-body inviscid supersonic flow of the numerical simulation. With NND format, by solving the
Interference
- 介绍了子母弹气动干扰风洞实验新方案的特点及实验装置的构成。利用该方案进行了布撒 器 —子弹气动干扰风洞实验。-Describes the shrapnel Aerodynamic wind tunnel tests of the new program features and the composition of experimental devices. Using the program was Dispenser- Bullet aerodynamic interference wi
qidongshiyan
- 非线性气动系统实验的源代码，使用滑膜控制的方法-Pneumatic system test source code
RGLS
- RGLS算法 系统辨识 实验的源程序代码 用于气动伺服实验-RGLS algorithm systems identification of the source code for the pneumatic servo test
8630
- 8630是国外生产的一款气动阀门，这份文档中详细地介绍了8630的使用说明和操作规范。-8630 is the foreign production of a pneumatic valve, this document describes in detail the use of the 8630 instructions and operating norms.