An approach that combines numerical, experimental, and theoretical analyses has been
implemented to investigate the effects of the injection parameters on the flame flashback …

High-enthalpy gas streams in a real engine or wind tunnel will contain some trace gases;
however, this is often ignored in many studies. To investigate transverse fuel-jet mixing and …

In this paper we enhance the well-known fifth order WENO shock-capturing scheme by
using deep learning techniques. This fine-tuning of an existing algorithm is implemented by …

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

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 …

In this paper, the cavity parameters of length-to-depth ratio, aft ramp angle, and nitrogen
throttling positions are numerically studied by a Large Eddy Simulation (LES) combined with …

This paper develops a new hybrid finite difference scheme which consists of a nonlinear
WENOCU4 scheme to maintain the numerical stability near discontinuities and a fourth …

This study investigates the flow structures and combustion regimes in an axisymmetric cavity-
based scramjet combustor with a total temperature of 1800 K and a high Reynolds number …

Under the guidance of the major two-period research program of the National Natural
Science Foundation of China, the hypersonic technique has steadily matured. Further …

In the present study, a fifth-order improved alternative weighted essentially non-oscillatory
scheme has been developed for nonlinear hyperbolic conservation laws. We have proposed …