Thermal System Oriented Simulation of Aircraft Electrical Environmental Control Systems Including its Electric Coupling
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Cita com:
hdl:2117/180119
Tipus de documentText en actes de congrés
Data publicació2019
EditorEuropean Conference for AeroSpace Sciences (EUCASS)
Condicions d'accésAccés obert
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Abstract
A flexible numerical platform based on libraries has been developed within the Dymola/Modelica framework to simulate Environmental Control Systems (ECS). The goal was to build up a flexible tool to analyse complex systems including their thermal and electrical perimeters at both steady and transient conditions focusing on three key characteristics: numerical robustness, optimal time consumption, and high accuracy. This document aims to underline both the most relevant features of the numerical tool and the main challenges addressed during its development. Some illustrative simulations are shown in order to highlight the tool capabilities.
CitacióAblanque, N. [et al.]. Thermal System Oriented Simulation of Aircraft Electrical Environmental Control Systems Including its Electric Coupling. A: European Conference for Aeronautics and Space Sciences. "8th European Conference for Aeronautics and Space Science (EUCASS): papers". European Conference for AeroSpace Sciences (EUCASS), 2019, p. 1-9.
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EUCASS2019-0767.pdf | 503,6Kb | Visualitza/Obre |