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Generally, the overall performance of scramjet combustor is greatly impacted by the fuel distribution scheme. The current paper mainly conducted a comprehensive parametric study of the impact of fuel distribution on the overall performance of a kerosene-based scramjet combustor. Herein, a 3D supersonic combustor with a recessed cavity and four injection orifices was taken into consideration. The combustor's performance was analyzed by 3D RANS model. The fuel equivalence ratio for each injectiondoi:10.1155/2016/7604279 fatcat:kj54hbwu2bbgrpw2jws74gad6a