Achieving efficient fuel-air mixing is a crucial problem for the design of scramjet engines.
Due to the very short residence time of the fuel within the scramjet combustor for typical flight …

The dual-mode scramjet combustor is a promising candidate for the combined cycle engine
of the hypersonic airplane, and the flame propagation and stabilization process in the dual …

The major hurdle in augmenting the performance of supersonic engines is the appropriate
distribution of injected fuel within the supersonic chamber. That's why SST k− ω model is …

Scramjets are regarded as one of the most efficient air-breathing propulsion devices in
supersonic flight conditions, and combustors are critical components in scramjet engines …

Achieving efficient fuel-air mixing is a crucial issue in the design of the scramjet engine due
to the compressibility effect on the mixing shear layer growth and the stringent flow …

The mixing process plays a very important role in the engineering realization of the scramjet
engine, and sufficient mixing between the incoming supersonic air and the fuel relates to …

In this study, the effects of the shock wave on sonic transverse hydrogen through single and
multi-jets for supersonic combustion were investigated numerically. This study presents the …

An effective fuel supply strategy with high mixing efficiency, large penetration depth and low
stagnation pressure losses determines the overall performance of the scramjet (supersonic …

Numerical investigation of some mixing enhancement strategies based on the traditional
transverse injection technique proposed in recent years was carried out by means of the …

A good injection strategy with high penetration and mixing efficiency relates to the overall
performance of the airbreathing hypersonic propulsion system. In the current study, the …