System Integration in Aircraft Environment - Hydraulic Performances through Coupled Simulations

被引:0
|
作者
Hutchison, Matthieu [1 ]
Marles, David [2 ]
Singh, Ashutosh [3 ]
Witt Lng, Henning [4 ]
Boulon, Pierre [5 ]
机构
[1] Airbus Operations SAS
[2] Airbus Operations UK
[3] Airbus Operations India
[4] Airbus Operations GmbH
[5] Chiastek Inc
关键词
Vehicle performance;
D O I
10.4271/2020-01-0004
中图分类号
学科分类号
摘要
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. © 2020 US Air Force Research Laboratory. All rights reserved.
引用
收藏
页码:1139 / 1149
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