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Facilities
2.4m Continuous Transonic Wind Tunnel (FL-62)
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2.4m Continuous Transonic Wind Tunnel (FL-62)
FL-62, a continuous high speed single circuit wind tunnel, mainly undertakes advanced research test and model test. It meets conventional force/pressure test requirements of advanced aircrafts of the next period of time, besides, catches up with international level of similar wind tunnels in the terms of overall capability.
Main Performance:
Test section size：2.4m×2.4m
Mach number：0.3~1.6
Total pressure: 0.03~0.4MPa
Total temperature: 293~333K
Max Reynolds number: 1.3×107
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1.5 m Trisonic Wind Tunnel (FL-3)