In this paper, mathematical model of fluctuating torques acting on rectangular super-tall buildings were investigated based on windtunnel test results.
利用风洞试验结果，对矩形截面超高层建筑风致脉动扭矩数学模型进行研究。
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The flow field of the wing tip vortex, which shed from a rectangular wing, is surveyed by a seven holes probe in a low speed windtunnel.
A study is carried out on a hypersonic inlet with rectangular-to-circular shape transition and forebody using numerical simulation and high enthalpy windtunnel test.