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首页> 外文期刊>International journal of aerospace engineering >Modeling of Spray Combustion with a Steady Laminar Flamelet Model in an Aeroengine Combustion Chamber Based on OpenFOAM
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Modeling of Spray Combustion with a Steady Laminar Flamelet Model in an Aeroengine Combustion Chamber Based on OpenFOAM

机译:基于OpenFOAM的航空发动机燃烧室内稳态层流小火焰模型的喷雾燃烧建模

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摘要

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.
机译:高性能航空发动机燃烧室的发展很大程度上取决于有效数值模型的准确性和可靠性。在目前的工作中,已经在OpenFOAM中开发了具有稳定层流小火焰模型和喷雾模型的反应求解器,并给出了求解器的详细信息。该求解器首先通过Sandia / ETH-Zurich火焰验证。此外,它还用于通过RANS方法模拟航空发动机燃烧室内的非预混合煤油/空气喷雾燃烧。与可用实验数据的比较显示出良好的一致性,并验证了OpenFOAM中新开发的求解器的功能。

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