The layout of the strut fuel injector has a significant impact on the flame stabilization process
of the strut-based scramjet combustor. That's why a two-strut-based scramjet model has …

A high-fidelity numerical solver, RYrhoCentralFoam, is developed based on OpenFOAM® to
simulate turbulent compressible reactive flows. It is designed for accurately simulating …

A brief review of the recent advances in kerosene-fueled supersonic combustion modeling is
present by comparing the fuels, reviewing the kinetic mechanisms, and introducing recent …

Insight into supersonic combustion characteristics of thermally cracked fuels in a scramjet
combustor is crucial for the development of next-generation supersonic flight vehicles. In the …

An ethylene-fueled scramjet operating at Mach 10 was experimentally tested in the JF-24
shock tunnel and modeled using improved delayed detached eddy simulation based on up …

A zonal nonequilibrium model (ZNM) based on the concept of zonal representation of the
nonequilibrium relaxation times is proposed. ZNM, together with dynamic zone flamelet …

With the help of an O 2-pilot strut, the stable supersonic combustion was achieved in a
scramjet combustor fueled by liquid kerosene. Objective of this work is to investigate the …

The uninstalled performance of a full-scale scramjet operating over Mach 7 to 10 and
altitudes of 28 to 40 km was numerically analyzed by using high-fidelity Improved Delayed …

A three-dimensional hybrid LES (Large Eddy Simulation)/RANS (Reynolds-averaged Navier–
Stokes) study dedicated to understanding the jet-wake flame stabilization under high inflow …

A control-oriented unsteady 1-D model for regeneratively-cooled scramjet engine which is
composed of flow-combustion module, regenerative cooling module, is presented in this …