Separated Computation of the Whole Jet Engine Workflow

Leonid Shabliy, Alexander Krivcov, Oleg Baturin

Abstract

The research goal was the methodology to calculate gas turbine engine (GTE) workflows and in the compressor, in the combustion chamber and the turbine at the same time. Our method allows predicting interactions between components of a GTE. Solution is provided in separate solvers step by step. The results of modeling entire GTE in a different CFD codes are presented. Efforts to decide some problem of matching models are written. Author shows the maximum accuracy of boundary data achieved with this approach.

References

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Paper Citation


in Harvard Style

Shabliy L., Krivcov A. and Baturin O. (2014). Separated Computation of the Whole Jet Engine Workflow . In Proceedings of the 4th International Conference on Simulation and Modeling Methodologies, Technologies and Applications - Volume 1: SIMULTECH, ISBN 978-989-758-038-3, pages 274-279. DOI: 10.5220/0005108602740279


in Bibtex Style

@conference{simultech14,
author={Leonid Shabliy and Alexander Krivcov and Oleg Baturin},
title={Separated Computation of the Whole Jet Engine Workflow},
booktitle={Proceedings of the 4th International Conference on Simulation and Modeling Methodologies, Technologies and Applications - Volume 1: SIMULTECH,},
year={2014},
pages={274-279},
publisher={SciTePress},
organization={INSTICC},
doi={10.5220/0005108602740279},
isbn={978-989-758-038-3},
}


in EndNote Style

TY - CONF
JO - Proceedings of the 4th International Conference on Simulation and Modeling Methodologies, Technologies and Applications - Volume 1: SIMULTECH,
TI - Separated Computation of the Whole Jet Engine Workflow
SN - 978-989-758-038-3
AU - Shabliy L.
AU - Krivcov A.
AU - Baturin O.
PY - 2014
SP - 274
EP - 279
DO - 10.5220/0005108602740279