Jet Engine Fuel System Integration in Aircraft Environment - Methodology for Pressure Surge Simulation through Model-Based System Engineering 2014-01-2135
An Airbus methodology for the assessment of accurate fuel pressure surge at early program stages in the complete aircraft and engine environment based on joint collaboration with LMS Engineering is presented. The aim is to comfort the prediction of the fuel pressure spike generated by an engine shutdown in order to avoid late airframe fuel system redesign and secure the aircraft entry-into-service.
Citation: Hutchison, M., Lenoble, G., Badiali, U., Sommerer, Y. et al., "Jet Engine Fuel System Integration in Aircraft Environment - Methodology for Pressure Surge Simulation through Model-Based System Engineering," SAE Int. J. Aerosp. 7(1):74-89, 2014, https://doi.org/10.4271/2014-01-2135. Download Citation
