Numerical investigation of transpiration cooling for sintered metal porous strut in a scramjet combu

来源 :2nd International Workshop on Heat Transfer Advances for Ene | 被引量 : 0次 | 上传用户:bkln81
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  Strut structure is designed to inject fuel into combustor in some scramjet engines, while the flow within the combustor and nozzle is always supersonic.Tremendous aerodynamic heating causes challenging design issues concerning the thermal protection of the strut.
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