Study of Supersonic Combustion Characteristics in a Scramjet Combustor

作者: Tarek Abdel-Salam , Surundra Tiwari , Tajeldin Mohieldin

DOI: 10.2514/6.2003-3550

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摘要: Numerical calculations have been performed to study the flowfield of a dual-mode scramjet combustor. Results are obtained with finite volume CFD code and using unstructured grids. A 3-D combustor has investigated two different types fuels. Only half physical domain solved by forcing symmetry condition at centerplane model. presented for hydrogen combustion ethylene combustion.

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