AeroEngineS Взлом 12.8.3

Скриншоты

Описание

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
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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

История обновлений

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

12.8.1

2021-09-07

-Design modifications

12.8.0

2021-08-30

- Atmosphere calculation 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

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

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.