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System Integration in Aircraft Environment - Hydraulic Performances through Coupled Simulations
ISSN: 2641-9637, e-ISSN: 2641-9645
Published March 10, 2020 by SAE International in United States
Citation: Hutchison, M., Marles, D., Singh, A., Witt lng, H. et al., "System Integration in Aircraft Environment - Hydraulic Performances through Coupled Simulations," SAE Int. J. Adv. & Curr. Prac. in Mobility 2(3):1139-1149, 2020, https://doi.org/10.4271/2020-01-0004.
An Airbus methodology for the assessment of accurate hydraulic performance at early program stages in the complete aircraft and power consuming systems environment based on joint collaboration with Chiastek is presented. The aim is to comfort the prediction of an aircraft hydraulic performance in order to limit the need for a physical integration test bench and extensive flight test campaign but also to avoid late system redesign based on robust early stage model based engineering and to secure the aircraft entry-into-service.