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0.6 m Trisonic Wind Tunnel (FL-7)


0.6 m Trisonic Wind Tunnel (FL-7)

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0.6 m Trisonic Wind Tunnel (FL-7)



FL-1, a half-return-circuit blow down trisonic wind tunnel built in 1958, is Chinese first industrial wind tunnel being regarded as “Meritorious Wind Tunnel”, and almost all types of Chinese aircrafts have been tested here.


Main Performance:


Test section size:0.6m×0.6m
Mach number:0.3~4.0



Conventional force test/pressure test, External Store force test, Hinge-moment test, Component force test, Aerated model force test, Air intake test, Dynamic derivative test, Half model supporting, Two dimensional airfoil test, PSP, TSP, IR , PIV, Schlieren etc.