1.
The Application of PIV Technology in Automotive Wind Tunnel
PIV技术在汽车模型风洞中的应用
2.
An Experimental Investigation of Xiling Changjiang Suspension Bridge Using Aeroelastic Models
西陵长江大桥全桥气动弹性模型风洞试验研究
3.
The Similarity Rules of Aeroelastic Model of High Pier Wind Tunnel Tests
桥梁高墩气动弹性模型风洞试验的相似律
4.
simulate flight using a model plane in a wind tunnel
用模型飞机在风洞里模拟飞行
5.
Modal Coupling Analysis of Long-span Bridge Model in Wind Tunnel Test
大跨桥梁风洞试验模型模态耦合分析
6.
Wind tunnel force balance test and wind-induced responses of the Guangzhou New TV Tower structure Ⅰ:wind tunnel test
广州新电视塔模型测力风洞试验及风致响应研究Ⅰ:风洞试验
7.
The Simulated Test of the Wind Erosion & Wind Tunnel on Wind Contour Characteristics Close to Ground Surface at Typical Wind Erosive Region;
典型风蚀地况近地表风廓特性的风洞模拟研究
8.
The Optimization of Wind Tunnel Simulative System on Wind Speed Contour Line of Typical Wind Erosive Ground Surface;
典型风蚀地表风速廓线风洞模拟系统的优化
9.
The Simulation of Wind Speed Contour Line of Typical Wind Erosion Surface in Wind-tunnel Based on Fluent
基于Fluent的风洞典型风蚀地表风速廓线的模拟
10.
Asummary of optics model displacement measuring technique application in wind tunnel
风洞模型位移光学测量技术应用综述
11.
Force-Measuring Experiment for the Scale Model of WDPSS in Low-Speed Wind Tunnel
WDPSS缩比模型的低速风洞测力试验
12.
Research on quantitative assessment model on vulnerability risk for information system
信息系统漏洞风险定量评估模型研究
13.
Studies on the Experiment in the Wind Tunnel and Numerical Simulation of the Sinusoidal Wind Spectrum;
正弦型风谱的风洞实验与数值模拟研究
14.
The measurement and control of the model attitude angle in airfoil wind tunnel test
翼型风洞实验模型姿态角的测量与控制
15.
Thermal Model Experimental Reaserch on Ventilation of Bus Corridor and Main Transformer Room of Hohhot Hydropower Station with 2D-PIV
呼和浩特水电站母线洞及主变洞热态通风模型2D-PIV试验研究
16.
Compressibility effects are investigated with highspeed models in high-speed tunnels.
压缩性影响需用高速模型在高速风洞中试验。
17.
Research on High Power Density Motor Used for Wind Tunnel Test of Propeller Aerocraft Model
飞机模型带动力风洞实验高功率密度电机研制
18.
4m×3m LOW-SPEED TUNNEL MODEL ATTITUDE ANGLE CONTROL SYSTEM
4米×3米低速风洞模型姿态角控制系统