Evaluation of flamelet/progress variable model for the applications in supersonic combustion using hybrid RANS/LES approach

Author:

Tang Tao,Wang HongboORCID,Sun Mingbo,Zhao Guoyan,Yu Jiangfei,Fan Zhouqin,Wang Zhenguo

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. Review of combustion stabilization for hypersonic airbreathing propulsion;Liu;Prog. Aerosp. Sci.,2020

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4. A consistent flamelet formulation for non-premixed combustion considering differential diffusion effects;Pitsch;Combust. Flame,1998

5. Investigation of flame flashback phenomenon in a supersonic crossflow with ethylene injection upstream of cavity flameholder;Zhao;Aerosp. Sci. Technol.,2019

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