Transonic Wind Tunnel
[ Testing Equipment ]

Transonic Wind Tunnel
To verify airflow characteristics of a jet plane etc., aerodynamic performance tests in regions of Mach number = 0.8 to 1.4 or so, are essential.
This facility is intended to test flight characteristics in the regions of Mach number = 0.8 to 1.4 or so. We have manufactured wind tunnels to achieve various Mach numbers corresponding to the test purposes.

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