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Improved thermal performance of cooling channels with truncated ribs for a scramjet combustor fueled by endothermic hydrocarbon

Truncated RibsEngineeringAerospace EngineeringCombustion ScienceThermal ManagementCombustion EngineeringThermodynamicsThermal PerformanceHeat TransferScramjet CombustorThermal EngineeringSupersonic Combustion