Wind tunnel is the main equipment in aerodynamic research. At present the test between Mach numbers 0 ~ 25, altitudes 0 ~ 90 Km can be performed by ground test equipment. A variety of tests can be done such as steady and unsteady test, static and dynamic test, low angle of attack to high angle of attack test, and so on.

In the future, large-scale wind tunnel, high reynolds number wind tunnel and high-energy equipment will be constructed. The simulation and test ability will leap forward.

              Plane Tremor Test                              Special Inlet Test