The purpose of this paper is to investigate the effect of impinging oblique shock on
combustion efficiency of hydrogen injection into the supersonic cross-flow. The two …

The aim of the present study is to analyze the attenuation of detonation waves in dust-free
and dusty air. The two-phase model for compressible reacting flow including chemically inert …

Heat addition due to exothermic reactions of ablated chromium in hypersonic flow on coated
blunt bodies is numerically investigated. The advection upstream splitting method is used as …

The purpose of this paper is to investigate the effects of intake's compression process of the
scramjet on its flight performance. The hydrogen injection to the supersonic cross-flow is …

Supersonic hydrogen–air cylindrical mixing layer is numerically analyzed to investigate the
effect of inlet swirl on ignition delay time in scramjets. Combustion is treated using detailed …

The purpose of the present work is to investigate the response of an evaporating and
decomposing droplet cloud to applied excitations in the surrounding. The classic and …

The gas dynamic laser is numerically studied using quasi-1D and 2D simulations to
investigate the effect of diamond pattern of the supersonic flow field (inhomogeneities in …

The most recent idea of using the exothermic coating to reduce the drag coefficient on blunt
noses in hypersonic flows is numerically simulated to study parametrically the effect of …

The liquid oxygen/methane staged cycle liquid-rocket engine is one of the most potential
rocket engines in the future for its higher performance, higher fuel density and reusable …