Modeling of Spray Combustion with a Steady Laminar Flamelet Model in an Aeroengine Combustion Chamber Based on OpenFOAM

Abstract EN

The development of high-performance aeroengine combustion chambers strongly depends on the accuracy and reliability of efficient numerical models.

In the present work, a reacting solver with a steady laminar flamelet model and spray model has been developed in OpenFOAM and the solver details are presented.

The solver is firstly validated by Sandia/ETH-Zurich flames.

Furthermore, it is used to simulate nonpremixed kerosene/air spray combustion in an aeroengine combustion chamber with the RANS method.

A comparison with available experimental data shows good agreement and validates the capability of the new developed solver in OpenFOAM.