Thermal System Oriented Simulation of Aircraft Electrical Environmental Control Systems Including its Electric Coupling
Document typeConference report
PublisherEuropean Conference for AeroSpace Sciences (EUCASS)
Rights accessOpen Access
All rights reserved. This work is protected by the corresponding intellectual and industrial property rights. Without prejudice to any existing legal exemptions, reproduction, distribution, public communication or transformation of this work are prohibited without permission of the copyright holder
ProjectMALET - Development of MODELICA Libraries for ECS and Thermal management architectures (EC-H2020-686783)
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.
CitationAblanque, 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.