# AeroEngineS

> Aircraft Engine Performance

Canonical page: [https://chrome-stats.com/d/id1451710013](https://chrome-stats.com/d/id1451710013)

## Overview

- **ID:** `id1451710013`
- **Platform:** Apple
- **Type:** Apple app
- **Status:** Available
- **Publisher:** Aristotle University of Thessaloniki
- **Category:** Education
- **Rating:** 5.00 / 5 (1 ratings)
- **Version:** 12.8.3
- **Last updated:** 2023-01-13
- **First published:** 2019-05-03
- **Size:** 7.43 MB
- **Data as of:** 2026-09-05
- **Store listing:** [Apple App Store](https://apps.apple.com/us/app/aeroengines/id1451710013)
- **Privacy policy:** [https://www.auth.gr/](https://www.auth.gr/)

## 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

## Rankings

- #753,374 — Overall
- #28 — engine

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Source: [Chrome-Stats](https://chrome-stats.com/d/id1451710013)