In this research, the effects of oblique shock on the mixing characteristics in a supersonic
combustor equipped with a cavity is numerically investigated. To reveal the flow structure of …

Supersonic shear layers experience instabilities that generate significant adverse effects; in
complex configurations, these instabilities have global impacts as they foster compounding …

The scale effect of flame flashbacks inside an ethylene-fueled scramjet combustor was
investigated through an approach that combines numerical, experimental, and theoretical …

The mixing process of a fuel jet in a supersonic crossflow is one of the significant issues for
the design of the scramjet combustor. In this paper, the orthogonal analysis was employed to …

The flow mixing mechanism between sonic fuel jet and supersonic mixed inflow is one of the
key technologies in rocket-based combined cycle engines. In this study, the flow mechanism …

In this study, the effect of boundary layer thickness on supersonic combustion in an ethylene-
fueled scramjet combustor under Mach 5.5 flight conditions is studied by employing …

The demanding working environment of hypersonic missiles imposes high requirements on
the reliability and stability of the reaction control system. This work aims to investigate the …

Large-eddy simulations and nanoparticle-based planar laser scattering experiments are
conducted to investigate various physical aspects of transverse sonic jets injected into a Ma …

In this work, the performance of secondary injection thrust vector control of an altitude
adaptive planar double divergent supersonic nozzle is numerically investigated. The …

During the operation of hypersonic vehicles, a reciprocal coupling effect is manifested
between the inlet and the combustion chamber. This results in an unavoidable non …