Features & Capabilities

Aircraft Engine Performance at Design Point

  • Subsonic/Supersonic 1-Spool Turbojet

  • Subsonic 2-Spool Turbofan

  • Subsonic 2-Spool Boosted 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

Hybrid Precooled Rocket Engine at Design Point

  • Analysis of the combined Thermodynamic Cycles with Air, Hydrogen & Helium as working fluids

Ramjet Engine at Design Point

  • Simulation of the thermodynamic cycle of a hydrogen-fuelled Ramjet engine at optimized conditions.

Ramjet Engine at Design Point

  • Simulation of the thermodynamic cycle of a hydrogen-fuelled Ramjet engine at optimized conditions.

Supersonic 2-spool Turbojet Engine at Design Point

  • Simulation of the thermodynamic cycle of a Supersonic 2-spool turbojet engine with reheat.

Aircraft Emissions

  • Emissions calculation for aircraft engines in LTO cycle and Cruise
  • Type of turbofan engines used: 1. Subsonic 2-Spool, 2. Subsonic 3-Spool

Compressor Map Operating Point Prediction using

  • Scaling Techniques on an existing HPC map
  • Artificial Neural Networks to interpolate the existing map's data

Developer: Aggelos Gaitanis Original creator: Evangelia Pontika HyRE, Ramjet tab programmer: Spiros Tsentis Supersonic 2-spool Reheated tab programmer: Anastasios Saflekos Emissions tab developer/programmer: Maria Bakali Advisor: Ioanna Aslanidou, Konstantinos Kyprianidis Supervisor: Anestis Kalfas

User Growth & Download Statistics

App
By:
Aristotle University of Thessaloniki
Rating:
5.00
(1)
5.00
Version:
12.8.3 Last updated: 2023-01-13
Version code:
854364457
Creation date:
2019-05-03
Compatible devices:
Size:
7.43MB
URLs:
Privacy policy
Full description:
See detailed description
Source:
Apple Apps Store
Data ingested on:
2026-06-07
Compare stats and ranking:

Contact the developer

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Developed by:
Aristotle University of Thessaloniki
Apple Apps Store
https://apps.apple.com/us/app/aeroengines/id1451710013

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