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This paper aims to describe the reasons why abnormal heat transfer occurs under the condition of regenerative cooling applied in scramjet engines. Supercritical n-decane flowing in a horizontal tube under various mass flow rates (G = 0.001, 0.002, 0.003, 0.004 kg/s) and heat fluxes (qw = 100, 200, 300, 400 kW/m2) is investigated by numerical simulations. The mechanisms of the abnormal heat transfe
