CORDIS Project
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This project develops a Modelica library for thermodynamic properties of gases and liquids used in aircraft, along with an Excel interface for plotting thermodynamic design diagrams. It aims to cover the full temperature and pressure ranges experienced by aircraft, addressing gaps in existing model libraries.
With this proposal, a Modelica library for thermodynamic properties of gases and liquids that are used as working media in aircraft, and an Excel interface to the same functions with plotting capabilities for typical thermodynamic design diagrams (Temperature-Entropy and Enthalpy-Entropy) shall be developed.
It is important that the complete temperature and pressure range experienced by aircraft is covered, from -60 deg Celsius to 200 deg Celsius, depending on the fluid.
The pressure range depen…
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