AeroEngineS APK
APK Version History
- Version
- 3.0.7 (30070)
- Architecture
- universal
- Release Date
- December 05, 2023
- Requirement
- Android 5.0+
Download [ 5.4 MB ]
Safe
- Version
- 3.0.4 (30040)
- Architecture
- universal
- Release Date
- December 05, 2023
- Requirement
- Android 5.0+
Download [ 5.8 MB ]
Safe
- Version
- 3.0.1 (30010)
- Architecture
- universal
- Release Date
- December 05, 2023
- Requirement
- Android 5.0+
Download [ 5.8 MB ]
Safe
- Version
- 2.1.3 (20103)
- Architecture
- universal
- Release Date
- December 05, 2023
- Requirement
- Android 4.4+
Download [ 3.9 MB ]
Safe
- Version
- 2.0.4 (20004)
- Architecture
- universal
- Release Date
- December 05, 2023
- Requirement
- Android 4.4+
Download [ 3.9 MB ]
Safe
About Radio FM 90s
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.
What's New in this version
Updated version to comply with Android policy