System Integration in Aircraft Environment - Hydraulic Performances through Coupled Simulations 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.
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. Download Citation
Author(s):
Matthieu Hutchison, David Marles, Ashutosh Singh, Henning Witt lng, Pierre Boulon
Affiliated:
Airbus Operations SAS, Airbus Operations UK, Airbus Operations India, Airbus Operations GmbH, Chiastek Inc
Pages: 11
Event:
AeroTech
ISSN:
2641-9637
e-ISSN:
2641-9645
Also in:
SAE International Journal of Advances and Current Practices in Mobility-V129-99EJ
Related Topics:
Vehicle integration
Flight tests
Aircraft
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