AeroEngineS

Aristotle University of Thessaloniki

Mayelana nalolu hlelo lokusebenza

Ukusebenza Kwenjini Yezindiza eMklamo Point
- I-Subsonic / Supersonic 1-Spool Turbojet
- I-Subsonic 2-Spool Turbofan
- I-Subsonic 2-Spool ekhuliswe iTurbofan
- I-Subsonic 3-Spool Turbofan

- Ukuhlaziywa kwe-Thermodynamic Cycle
- Indawo ye-Nozzle kanye nokusebenza (ukuqina, amandla njll.) Ukubalwa
- Ukugeleza Kwama-Mass (Core, Bypass, Fuel)
- Ukubalwa kwe-othomathikhi kwezimo ezisetshenziswayo kususelwa ekuphakameni kwendiza kusetshenziswa imodeli ye-International Standard Atmosphere
- Ukubalwa okuzenzakalelayo kweCp, igama, R kwisakhi ngasinye esuselwa emazingeni okushisa kanye neFuel to Air Ratio
- Ukubalwa okuzenzakalelayo kokusebenza kahle kwe-isentropic kwe-compressor ngayinye kanye ne-turbine ngokusekelwe ekusebenzeni kahle kwe-polytropic kanye nengcindezi yesilinganiso

I-Compressor Map Operating Point Prediction usebenzisa
- Amasu wokulinganisa kumephu ye-HPC ekhona
- Amanethiwekhi Wokuhlangana Kwasekhaya ukuze ahumushe imininingwane yemephu ekhona

Ukukhipha Izindiza
- Ukubalwa kwe-Emissions izinjini zezindiza emjikelezweni we-LTO kanye ne-Cruise
- Uhlobo lwezinjini ze-turbofan ezisetshenzisiwe: 1. Subsonic 2-Spool, 2. Subsonic 3-Spool

I-Hybrid Precooled Rocket Injini eDizayini Point
- Ukuhlaziywa kwemijikelezo ye-Thermodynamic ehlanganisiwe ne-Air, Hydrogen ne-Helium njengamanzi osebenzayo.

Yini entsha

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