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Detailed parametric investigations on drag and heat flux reduction induced by a combinational spike and opposing jet concept in hypersonic flows

Heat Flux ReductionUnsteady FlowParametric InvestigationsEngineeringAerospace EngineeringFluid MechanicsTurbulence ModelingAerodynamicsPropulsionHypersonic PropulsionHypersonic FlowSupersonic CombustionCombinational Spike