wind tunnels

TESTING A database management system for low speed wind tunnels

低速风洞试验数据库系统

Designs and manufactures turbine engine test cells and wind tunnels .

设计生产涡轮发动机测试单元和风洞。

Both types of tests have been explored in wind tunnels .

这两种形式的试验都已在风洞中进行过探索。

Aeronautical engineers take their models into wind tunnels to measure performance factors .

航空学工程师将他们的模型放置在风道内来测量性能因素。

Finite - Rate Water Vapor Condensation in Combustion - Heated Wind Tunnels

燃烧加热风洞中有限速率的水蒸气的凝结

On the applications and development of cryogenic wind tunnels

低温风洞应用与发展探讨

The experimental investigation of unsteady complex flow fields in wind tunnels requires advanced measurement techniques .

风洞中非定常复杂流场的实验研究要求先进的测量技术。

Wind tunnels in general are used for testing purposes and aerodynamical optimization .

译文风洞大体上讲是用来得到测试试验结果和空气动力的最佳化。

Design technique of advanced transonic wind tunnels

先进跨声速风洞的设计技术

Design of New Wire-driven Parallel Kinematic Manipulator for Wind Tunnels

一种用于风洞的新型柔索驱动并联机构设计

Investigation of dynamic test technology for a model pitching oscillation with large amplitude in high speed wind tunnels

高速风洞大振幅俯仰动态试验技术研究

A New Method to Correct Sidewall Interference in Two Dimensional Wind Tunnels & A Local Correction Approach

一种新型二元风洞侧壁干扰修正方法&当地修正法

On the correlation of force test results of a tactical missile calibration model in five different wind tunnels

战术导弹标模五座风洞试验数据的相关性研究

Characteristics of ultra-low speed wind tunnels for research on Micro-UAV

微型飞行器研究用极低速风洞的特点

Sidewall Effects of Wind Tunnels on Velocity Profiles in Blown-Sand Flow

风洞边壁对挟沙气流流速分布的影响

A new concept of Parallel Wire Driven Robot applied in wind tunnels experimentation is recently presented .

将PWDR应用于风洞试验是近年来提出的一个新概念。

It is now common practice to test scale models of bridges in wind tunnels for aerodynamic resistance .

现在的通常作法是按比例缩小的桥梁模型放在风洞里检测它们的空气动力抵抗力。

An engineering correction method for tunnel wall interference and STING-SUPPORT interference in high speed wind tunnels

高速风洞洞壁干扰和支架干扰的工程修正方法

Measurements of fiow unsteadiness and its influence on experimental data in high speed wind tunnels

高速风洞气流脉动的测量及其影响

Hypersonic wind tunnels operating at very low densities were developed starting in about 1960 .

低密度超音速风洞大约开始发展于1960年。

The exploration of a new kind of free-released balance in impulsive wind tunnels

脉冲风洞中新型自由天平探索

On the modification of the correction rule for sidewall interference in two-dimensional wind tunnels

二维风洞侧壁干扰修正准则的改进

It 's an important advance for jet simulation to simulate hot jet by cryogenic wind tunnels .

应用低温风洞模拟热喷流，是喷流模拟技术一大进步。

A Design for Contraction Sections of Two-Dimensional High-Subsonic Wind Tunnels

高亚声速二维风洞收缩段的设计

Screens and metal grids are commonly used to adjust the flow in the design of wind tunnels .

风洞设计中，普遍采用孔板、金属网等构件进行整流。

Experimental results show a promising prospect for utilizing the injector driven technique in advanced transonic wind tunnels .

实验研究还表明引射驱动方式应用于跨音速风洞具有光明的前景。

Discussion on the simulation of atmospheric boundary layer with spires and roughness elements in wind tunnels ;

动态风荷载测试数据的可靠性依赖于大气边界层流场的正确模拟。

Design Methodology of Wire-Driven Parallel Support Systems in the Low Speed Wind Tunnels and Attitude Control Scheme of the Scale Model

低速风洞绳牵引并联支撑系统的机构与模型姿态控制方案设计

A group of the moderate and desirable size of wind tunnels at different speed range is recommended for reference .

文中推荐了不同速度下一组较合适的且能满足需要的风洞尺寸，供人们参考。

Overview of Wire-driven Parallel Kinematic Manipulators for Aircraft Wind Tunnels

应用于飞行器风洞试验的绳牵引并联机构技术综述