1.
Study on Undisturbed Cultivated Land Erosion Character by Erosion Wind Tunnel;
利用风蚀风洞研究原状农田土样的风蚀特性
2.
A Numerical Wind Tunnel Study on Distance between Tail Wing and Rear Hood and Angle of Attack of Tail Wing of a Car Model Using CFD;
轿车尾翼间隙和攻角的数值风洞研究
3.
Experimental study of along-wind response and across-wind response by aeroelastic model
横风向与顺风向动态风荷载的风洞试验研究
4.
Test Study on Windproof Net for Coal Storage Yard of Qinhuangdao Harbor
秦皇岛港煤堆场防风网风洞试验研究
5.
Research on Wind Speed Control System for Wind Tunnel Based on PLC;
基于PLC的风洞风速调控系统的研究
6.
A WIND TUNNEL EXPERIMENTAL STUDY ON THE OVERLAP RATIO OF SAVONIUS ROTORS
Savonius风力机叶片重叠比的风洞实验研究
7.
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
8.
On the Phenomenon of Origination and Weathering of Speleothem in Baiyundong in Lincheng County of Hebei Province;
河北临城白云洞洞积石形成与风化现象研究
9.
A Wind Tunnel Test and Research on Blades of the Concentrated Wind Energy Turbine;
浓缩风能型风力发电机叶轮的风洞实验与研究
10.
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
11.
The Design and Experimental Studies of Supersonic Straight Through Wind Tunnel and "Supersonic-supersonic" Mixing Layer Wind Tunnel;
直连式超声速风洞与“超—超”混合层风洞的设计和实验研究
12.
Experimental Investigation of the Cooling Performance of Tailrace Tunnel Ventilation in Hydropower Stations;
水电站无压尾水洞引风换热试验研究
13.
The Test Technology Research of the High Enthalpy Free-piston Shock Tunnel;
高焓自由活塞激波风洞试验技术研究
14.
A Study of Blunted-Wedge Holder and It s Application in CARDC s Arc-Heated Wind Tunnel;
电弧风洞钝楔试验技术及其应用研究
15.
The Research of Risk Management to Power House and Tunnel Project;
XX水电站“厂房隧洞工程”风险管理研究
16.
Research on Ventilation for Large Scale Underground Cavity Groups Construction;
大型地下工程洞室群施工期通风研究
17.
Research on operation and management of NASA's wind tunnel testing facilities
NASA风洞试验设备运行与管理研究
18.
Wind Tunnel Investigation on Dynamic behavior of 80°/65° Double Delta Wing in Rolling at High Incidence
80°/65°双三角翼摇滚特性风洞实验研究