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Closed-circuit wind tunnel Transonic
aeronautical

closed-circuit wind tunnel
closed-circuit wind tunnel
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Characteristics

Other characteristics
closed-circuit
Other characteristics
aeronautical
Temperature

Min.: -10 °C
(14 °F)

Max.: 180 °C
(356 °F)

Description

Since 1956 ARA has provided wind tunnel data of the highest quality by developing and utilising highly efficient, world-class techniques for our global civil and military aerospace customer base.The ARA Transonic Wind Tunnel (TWT) is a closed circuit, continuous flow tunnel with the following operational features;Test section: 2.74m wide x 2.44m high (9ft x 8ft).Four porous walls 22% maximum porosity.Mach number: 0 to 1.4Stagnation pressure: 0.8 to 1.2 atmospheres (standard operation is 1 atmosphere)Reynolds number: 3.5 to 16.7 million/m (dependent upon Mach number)

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*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.