Fuel injection strategies and vortex generators (VGs) play vital roles in effectively managing
temperature distribution within the combustion chamber of scramjet engines. By optimizing …

This work presents a comprehensive framework for the efficient implementation of finite-
volume-based reacting flow solvers, specifically tailored for high speed propulsion …

The novel dorsal intake hypersonic configuration has become a research hotspot in the
aerospace industry due to its superior aerodynamic and inlet performance at small angles of …

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

The cavity-assisted scramjet has been proven to be the most promising propulsion system
for air-breathing hypersonic vehicles. In this paper, numerical simulations of a Mach 8 …

The advent of data-based modeling has provided new methods and algorithms for analyzing
the complex flow fields in high-speed combustion applications. These techniques can be …

Accurately predicting turbulent combustion processes is fundamental for optimizing
efficiency, reducing pollutant emissions, and ensuring operational safety in combustion …

Most sub-grid scale (SGS) models employed in LES (large eddy simulation) formulations
were originally developed for incompressible, single phase, inert flows and assume transfer …

An approach based on the OpenFOAM library has been developed to solve a high-speed,
multicomponent mixture of a reacting, compressible flow. This work presents comprehensive …

Air vehicles have began to develop with advancing technology. In order to increase the
thrust and reduce pollutant levels at high speeds, researchers focus on different combustion …