The airline of the wind tunnel test center is a transitional structure,including a transition from a square to a circle and a transition from a circle to a square,which is very different from ordinary buildings.

The wind tunnel experiment techniques of backward dispersion of turning shrapnel;

Design-oriented wind tunnel experiments for house buildings;

The wind tunnel experiment of the hot spring swimming center in Jiuzhaigou International Convention and Vacation Center was carried out to investigate the structure behavior under wind loads.

Numerical simulation application in the wind tunnel test on Chongqing Grand Theater model;

Study on rain-wind induced vibration of cables in cable-stayed bridges by wind tunnel test;

Method of selecting high-speed train scale model for wind tunnel testing of aerodynamic drag based on numerical computation;

In response to the present condition that the MSS anti-wind study is less at domestic and,basedon the wind-tunnel testing and research of Pearl River Huang-Pu Bridge MSS62.

Through wind-tunnel tests,the longitudinal and lateral aerodynamic force and moment characteristics and static stabilities are compared with them after mounting of the lifesaving system in terms of different angle-of-attacks,sideslip angles and wind speeds,and finally the eff.

This paper introduces several kinds of experimental methods such as wind-tunnel test of a warship model wake field, warship model flow figure test, simulation test on the ground of flow field over the warship surface and a part of experimental resu.

The wind tunnel tests are only performed in the uniform flow, and the inflow wind angle, when the wind direction is transverse to bridge, is defined as 0°.

The aerodynamic parameters of Wuhu Bridge over the Yangtze River and a high speed running on it were measured respectively by wind tunnel tests.

Aerodynamic analysis and wind tunnel testing on maglev launch assist;

In this study,a wind tunnel testing is first proposed using a segmental rigid model of transmission towers.

If we make a wing model which is similar to sliding mass,we can determine aerodynamic parameters by the wind tunnel testing and thus calculate the lift.