In this work, supersonic hydrogen combustion in the Hyshot II scramjet engine is
investigated. In particular, fundamental physics of mixing, combustion and vorticity …

Various forms of numerical shock instabilities are known to plague many contact and shear
preserving approximate Riemann solvers, including the popular Harten-Lax-van Leer with …

It is well known that low diffusion Riemann solvers with minimal smearing on contact and
shear waves are vulnerable to shock instability problems, including the carbuncle …

Many researchers have reported failures of the approximate Riemann solvers in the
presence of strong shock. This is believed to be due to perturbation transfer in the transverse …

Abstract The Harten–Lax–van Leer with contact (HLLC) approximate Riemann solver is
known to be plagued by various forms of numerical shock instability. In this paper, we …

L'objectif de ce travail est le développement d'un modèle et d'une méthode numérique
adaptés à la simulation duruissellement d'eau de pluie sur des surfaces agricoles. Pour …

A simple, robust, and accurate HLLC‐type Riemann solver for the compressible Euler
equations at various Mach numbers is built. To cure shock instability of the HLLC solver at …

The present study numerically investigates the combustion characteristics and performance
of a direct-connect gaseous hydrogen-fueled scramjet combustor depending on the injector …

The simple low‐dissipation advection upwind splitting method (SLAU) scheme is a
parameter‐free, low‐dissipation upwind scheme that has been applied in a wide range of …

Understanding and accurately modeling combustion processes in engines across a wide
range of operating conditions is critical for advancing both subsonic and supersonic …