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.


    Access

    Download


    Export, share and cite



    Title :

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


    Contributors:
    Yinli Xiao (author) / Zupeng Wang (author) / Zhengxin Lai (author) / Wenyan Song (author)


    Publication date :

    2018




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    Spray Flamelet Modeling of Kerosene Spray Combustion

    Yi, Ran / Zhang, Xu / Yang, Tao et al. | AIAA | 2019


    SPRAY FLAMELET MODELING OF KEROSENE SPRAY COMBUSTION

    Yi, Ran / Zhang, Xu / Yang, Tao et al. | TIBKAT | 2019


    Two-Zone Flamelet Combustion Model

    Chen, Changyou / Bardsley, Mark E. A. / Johns, Richard J. R. | SAE Technical Papers | 2000


    Improved Flamelet Modeling of Supersonic Combustion

    Ladeinde, Foluso / Lou, Zhipeng | AIAA | 2018


    Two-zone flamelet combustion model

    Chen,C. / Bardley,M.E. / Johns,R.J. et al. | Automotive engineering | 2000