An ethylene-fueled scramjet operating at Mach 10 was experimentally tested in the JF-24
shock tunnel and modeled using improved delayed detached eddy simulation based on up …

The paper presents the results of an experimental and numerical study on the combustion
characteristics of a supersonic combustor operation enhanced by pilot hydrogen and air …

The characteristics of a hydrogen jet flame in a one-sided divergent scramjet combustor are
investigated using both experiments and large-eddy simulations. Optical observations …

The characteristics of combustion flow fields and performance for hypersonic M12-02
scramjet were numerically simulated and analyzed. The compressible two-equation kw SST …

A numerical study of the ground testing of a hydrogen-fueled scramjet engine was
undertaken using the commercial computational-fluid-dynamics code CFD++. The simulated …

Efficient combustion without damaging the inlet state is the key to achieve stable operation
in the engine. In the present study, effect of the heat release distribution on the component …

Combining pylon injector with rocket is an effective method to achieve efficient mixing and
combustion in the RBCC engine. This study designs a fuel pylon with active cooling …

A hypersonic expansion tube facility was designed and constructed to primarily study
supersonic combustion phenomena. This paper provides an overview of the range of …

Scramjet engines are limited in performance due to engine starting problems at low
hypersonic speeds. For an accelerating hypersonic vehicle, intake contraction ratios are …

Oblique detonation engines (ODE) have significant potential for hypersonic propulsion, yet
there is a paucity of research investigating internal injection ODEs. In this study, a numerical …