AeroEngineS Hack 12.8.3 + Redeem Codes
Aircraft Engine Performance
Developer: Aristotle University of Thessaloniki
Category: Education
Price: Free
Version: 12.8.3
ID: gr.auth.meng.AeroEngineS
Screenshots
Description
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
- 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
Version history
12.8.3
2023-01-13
A new engine model was developed called "Supersonic 2-spool reheated engine"
12.8.2
2022-02-08
- Code refinement
- Bugs fixed
- Bugs fixed
12.8.1
2021-09-07
-Design modifications
12.8.0
2021-08-30
- Atmosphere calculation tab
- Turboramjet engine performance tab
- Turboramjet engine performance tab
12.7.9
2021-05-26
Update the preview screenshots
12.7.8
2021-05-24
New logo update
12.7.6
2021-02-03
Bug fixes in Total emissions calculation
12.7.5
2021-01-31
Emissions tab design improvements
12.7.4
2021-01-29
Design improvements
12.7.3
2021-01-28
- Design improvements
12.7.2
2021-01-27
- iPad design improvements
12.7.1
2021-01-25
- Design improvements after feedback from the users.
12.7.0
2021-01-24
- Bug fixes in the LTO emissions & Total emission calculation
- Design improvements
- Design improvements
12.6.8
2021-01-24
Design improvements
12.6.7
2021-01-23
In this version several changes have been made:
- Developer improvements:
1. The build method has changed using Capacitor native runtime platform.
2. The design has significantly improved to provide a high quality experience to the user.
- Tool capabilities:
1. The "Ramjet section" is added in the dashboard which calculates the performance of a ramjet engine at design point
- Developer improvements:
1. The build method has changed using Capacitor native runtime platform.
2. The design has significantly improved to provide a high quality experience to the user.
- Tool capabilities:
1. The "Ramjet section" is added in the dashboard which calculates the performance of a ramjet engine at design point
12.6.6
2020-06-23
The code of the Hybrid Rocket Engine has been updated in order to calculate the conditions and performance in the ByPass.
12.6.5
2020-06-20
The interface of the application was updated to meet the display requirements of iPhone X.
12.6.4
2020-06-16
The interface of the application was updated to meet the display requirements of iPhone X.
12.6.3
2020-06-12
The interface of the application was updated and several bugs have been fixed.
12.6.2
2020-06-05
The interface of the application was updated and several bugs have been fixed.
12.6
2020-06-03
The interface of the application was updated and several bugs have been fixed.
12.5
2020-05-30
The interface of the application was updated and several bugs have been fixed.
12.4
2020-05-25
At first, the interface of the application was updated. Two brand new sections, which calculate the distance between airports and the design point of a hybrid rocket engine, are also included.
12.3
2020-05-10
At first, the interface of the application was updated. A new tab was created which simulates the cycle of a two-spool turbofan engine with booster. Also, a button was added in the Results section of Turbofan simulations that informs the pressure condtions in the engine's nozzles (Core & Bypass nozzle). Finally, a brand new section is added, which calculates the emissions produced by aircraft engines in two main modes for the following pollutants: NOx, SOx, CO, HC, CO2.
12.2
2019-05-23
The code is modified to simulate more accurately the inlet mass flow of the engine and the combustion chamber.
Ways to hack AeroEngineS
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