Supersonic Wind Tunnel

Overview

A supersonic wind tunnel refers to a wind tunnel where the Mach number M of the airflow in the experimental section of the wind tunnel is between 1.4 and 5. The supersonic wind tunnel experiment is an indispensable part in the development of the aircraft. It not only plays an important role in the research and development of aviation and aerospace engineering, but also is indispensable in the fields of transportation, housing construction, and wind energy utilization with the development of industrial aerodynamics. With this experimental method, the flow conditions are easily controlled. During the experiment, the model or object is often fixed in the wind tunnel for repeated blowing, and the experimental data is obtained through the measurement and control instruments and equipment. Supersonic wind tunnel Design and development Supersonic wind tunnel facility Supersonic wind tunnel experiment and test

Compatible aircraft

This part fits the following platforms.

Fitment data pending — contact us with your aircraft model.

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