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 and Performance (Thrust, Power etc.) calculation
-Mass Flows (Core, Bypass, Fuel)
-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 maps data
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This app was developed as part of a thesis at Aristotle University of Thessaloniki
Developer: Evangelia Pontika, Dipl.- Ιng.
Supervisor: Anestis Kalfas, Dipl.- Ιng. PhD
web app link: http://aes.propulsion.gr