28th Congress of the International Council of the Aeronautical Sciences, 23 - 28 September 2012, Brisbane, Australia
EXPERIMENTAL INVESTIGATIONS OF HYDRAULIC DEVICES PERFORMANCE IN AVIATION ENGINE COMPARTMENT
G. K. Vedeshkin, A. Dubovitskiy, D. Bondarenko*, O. Verseux**
CIAM, Russian Federation; *EADS, Russian Federation; **AIRBUS, France
Keywords: hydraulic devices, engine compartment, vent components, discharge coefficients
The paper presents experimental investigations of discharge coefficients for the aviation engine compartment hydraulic devices. Vent inlets, vent outlets and compartment ventilation system had been investigated. Investigations had been performed with simulation of the fan flow over the engine hydraulic devices in the range M <= 0.2 …0.5.
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