- 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.
Recent changes: Updated version to comply with Android policy
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Don't be afraid to get as technical as need be. Turbine engines are extremely complex, and it might help to prepare users of this app who might be considering propulsion engineering as a career. Otherwise, great work! I'm an aerospace engineer, and I love the app. Keep it up! Jason Sampler WamplerAdvancedCommercial Aerospace
★★★★★Dawud Hassan· Feb 3, 2021
I think it is possible to make everything with plasma energy clay
★★★★☆Tom J· Sep 28, 2024
Impressive app, I'm a professional in the industry and there's a lot of good stuff in here, but a couple of things were at least labeled incorrectly. The engine diagrams used in the design point calculations use incorrect station numbers. Station 3 is always the inlet to the combustor, but the 2+ spool engines label station 3 to be the inlet to the compressor section after the Fan. Outside of that, this is a pretty cool app
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