In this paper, we present a methodology to integrated simulation of gas turbine engine (GTE). This method allow to predict performance of GTE components workflows with account the mutual influence. Steady state CFD modeling of compressor, combustion chamber and the turbine are demonstrated. Solution is provided in separate solvers step by step. Efforts to decide some problem of matching models are written. Author shows the accuracy level of boundary data achieved with this approach.

Volume Subject Area:
Multidisciplinary Design Approaches, Optimization and Uncertainty Quantification
Topics:
Simulation, Combustion chambers, Compressors, Computational fluid dynamics, Gas turbines, Modeling, Steady state, Turbines, Workflow
This content is only available via PDF.
Copyright © 2014 by ASME
You do not currently have access to this content.