AeroEngineS
AeroEngineS APK
3.0.10 ․ 4 months agoFree ․ Aristotle University of Thessaloniki ⇣ Download APK (9.54 MB)
Aircraft Engine Performance at Design Point
What's AeroEngineS APK?
AeroEngineS is a app for Android, It's developed by Aristotle University of Thessaloniki author.
First released on google play in 4 years ago and latest version released in 4 months ago.
This app has 2.5K download times on Google play and rated as 4.86 stars with 37 rated times.
This product is an app in Tools category. More infomartion of AeroEngineS on google play
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
Compressor Map Operating Point Prediction using
- Scaling Techniques on an existing HPC map
- Artificial Neural Networks to interpolate the existing map's data
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
Hybrid Precooled Rocket Engine at Design Point
- Analysis of the combined Thermodynamic Cycles with Air, Hydrogen & Helium as working fluids.
- 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
Compressor Map Operating Point Prediction using
- Scaling Techniques on an existing HPC map
- Artificial Neural Networks to interpolate the existing map's data
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
Hybrid Precooled Rocket Engine at Design Point
- Analysis of the combined Thermodynamic Cycles with Air, Hydrogen & Helium as working fluids.
