Separated computation of the whole jet engine workflow

Separated computation of the whole jet engine workflow

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 r...

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Bibliographic Details
Published in:2014 4th International Conference On Simulation And Modeling Methodologies, Technologies And Applications (SIMULTECH) pp. 274 - 279
Main Authors: Shabliy, Leonid, Krivcov, Alexander, Baturin, Oleg
Format: Conference Proceeding
Language:English
Published: SCITEPRESS 01-08-2014
Subjects:
Atmospheric modeling
Boundary Conditions
Combustion
Computational Fluid Dynamic
Computational modeling
Engines
Fluids
Fuels
Gas Turbine Engine
Power Balance
Related Workflow
Turbines
Turbulence Model
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Summary: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.
DOI:10.5220/0005108602740279