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Air Intake Test


Air Intake Test





Low speed wind tunnel(FL-8) and high speed wind tunnels(FL-1, FL-2, FL-3) in AVICARI are equipped with advanced dynamic and static acquisition equipment, high angle of attack and high sideslip angle mechanism, inlet eject pipe system, inlet vacuum suction pipe system, inlet flux control measurement system and inlet micro-jet, suction flow control pipe system. with perfect facilities and matured technology, AVICARI can provide customers with wind tunnel services like inlet performance measurement and analysis, advanced dynamic and static data measurement, accurate flux measurement, inlet surge characteristics evaluation, inlet and engine matching test with small size thrust device and real ignition device, inlet wind tunnel test within Mach number range of 2.0~4.0, inlet flow control test, special inlet wind tunnel test (such as carrier environmental control ventilation cooling system, NACA inlet test and engine APU intake system test) and pipe flow flowfield display.

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