Reynolds-Averaged Navier-Stokes simulations using kw model are employed to explore a
single cavity flame-holding configuration of an analogous supersonic combustor. The flight …

Abstract Reynolds-Averaged Navier-Stokes simulations using a kw model are employed to
explore a single cavity flame-holding configuration of an analogous supersonic combustor …

Abstract Reynolds-Averaged Navier-Stokes simulations using a k-ω model are employed to
explore an analogous supersonic combustor configuration with a single cavity flame …

ABSTRACT Sustaining the Supersonic Combustion in Scramjet engine is a very challenging
topic of research nowadays.'Singlestage-to-orbit'aerospace vehicles incorporating scramjet …

The air‐breathing engines, commonly known as Supersonic Combustor Ramjet
(SCRAMJET) engines, are one of the most prominent technologies among researchers due …

High-fidelity simulations with a validated methodology are employed to explore the physical
processes associated with different injection strategies on supersonic combustion. The …

A numerical investigation of a cavity-based supersonic combustor with non-reacting
upstream hydrogen fuel injection is conducted to study the effects of inlet Mach number (Ma) …

ABSTRACT CFD analysis of supersonic combustion of air with hydrogen fuel has been
performed for a scramjet engine. As the combustion is taking place at supersonic speeds …

Direct injection into a cavity-based supersonic ramjet combustor has been recently
considered to be an effective way of stabilizing the flame over a wide range of operating …

This paper presents the effect of cavity-based injection in an axisymmetric supersonic
combustor using numerical investigation. An axisymmetric cavity-based angled and …