AeroEngineS

Aircraft Engine Simulation & Compressor Map Operating Point Prediction

Aircraft Engine Simulation at Design Point

-Subsonic/Supersonic 1-Spool Turbojet

-Subsonic 2-Spool Turbofan

-Subsonic 3-Spool Turbofan

-Analysis of the Thermodynamic Cycle

-Nozzle Area & Performance (Thrust, Power etc.) calculation

-Automatic calculation of ambient conditions based on the flight altitude using the International Standard Atmosphere model

-Automatic calculation of Cp, gama, R for each component based on temperature and Fuel to Air Ratio

-Automatic calculation of isentropic efficiency for each compressor and turbine based on polytropic efficiency and pressure ratio

Compressor Map Operating Point Prediction using

-Scaling Techniques on an existing HPC map

-Artificial Neural Networks to interpolate the existing map's data

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This app was developed as part of a thesis at Aristotle University of Thessaloniki

Developer: Evangelia Pontika, Dipl.-Ing.

Supervisor: Anestis Kalfas, Dipl.-Ing. PhD

web app link: http://aes.propulsion.gr/