Application and theoretical analysis of the flamelet model for supersonic turbulent combustion flows in the scramjet engine

DOI10.1080/13647830.2014.962617OpenAlexW2030125660MaRDI QIDQ5071068

ZhenXun Gao, Chongwen Jiang, Jingying Wang, Chun Hian Lee

Publication date: 19 April 2022

Published in: Combustion Theory and Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/13647830.2014.962617

zbMATH Keywords

compressibility effectscramjet engineflamelet modelsupersonic turbulent combustionfinite rate model

Mathematics Subject Classification ID

Fluid mechanics (76-XX) Thermodynamics and heat transfer (80Axx)

Related Items (1)

On the ambiguity of premixed flame thickness definition of highly pre-heated mixtures and its implication on turbulent combustion regimes

Uses Software

• CHEMKIN

Cites Work

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• Numerical research on mixing characteristics of different injection schemes for supersonic transverse jet
• A numerical study of turbulent combustion characteristics in a combustion chamber of a scramjet engine
• Theoretical analysis of flamelet model for supersonic turbulent combustion
• Towards the ultimate conservative difference scheme. V. A second-order sequel to Godunov's method
• Direct numerical simulation of hypersonic turbulent boundary layers. Part 4. Effect of high enthalpy
• An Accurate and Robust Flux Splitting Scheme for Shock and Contact Discontinuities
• Turbulent Combustion
• Numerical investigation of turbulent hydrogen combustion in a SCRAMJET using flamelet modeling

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