AeroEngineS

Aircraft Engine Performance

Разработчик: Aristotle University of Thessaloniki
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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
______________________________________________________
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
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AeroEngineS Отзывы Пользователей

Innovative Application

Kampe on

Греция

Quite an innovative idea to model and calculate the characteristics of aero engines ! The application environment is user friendly and it provides fast calculations for otherwise hard to find data . Would recommend.

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AeroEngineS Конкуренты

Name
N/A
N/A
EASA Part 66 Exam Trainer
Aircraft Maintenance Engineers
Aerospace by AZoNetwork
Wind Turbine Generator
Aerogenerator
PhyCAI - Physics Simulation
Computer Aided Instruction
ATA Chapters reference
Airfoil Design
ONELAB
Finite Element Solver
Rolls-Royce MyAeroengine
JetTurbineRocketEngine
Plane Turbine Cryogenic Engine

AeroEngineS Установки

30дн.

AeroEngineS Доход

30дн.

AeroEngineS Доходы и Загрузки

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