The combustion occurs at supersonic velocities in a scramjet engine. Since the mixing and
combustion take place at high velocities, analyzing the mixing of air and fuel in the engine is …

This study aims to understand the flow performance of a dual wall-mounted cavities in a strut-
injector mounted scramjet combustor for steady-state and transient reacting conditions …

This work presents the numerical analysis of the DLR scramjet combustor for different jet
schemes of the double-nozzle injector, namely the various injection directions, injection …

To analyze the complex spatiotemporal evolution law of the high-speed jet flow field in a
liquid-ring pump ejector, both the classic and spectral proper orthogonal decomposition …

Mixing fuel and air in a scramjet combustor is one of the key challenges in its development
due to the short residence time available. Strut based injection is considered a viable …

Partially or completely reusing launch vehicles significantly reduces expenses for
manufacturing and testing in space missions. Thus, Reusable Launch Vehicles (RLV) can …

The liquid jet diffusion characteristics effected with evaporation process and the
mathematical representation of penetration depth in supersonic crossflow were discussed in …

Combustion characteristics in a scramjet combustor equipped with a thin strut were
observed and discussed in this paper. A series of numerical simulations were carried out …

Numerical investigation of Scramjet combustor is performed with the help of center lobed
strut to act as a parallel fuel injector. The geometry of the combustor plays a major role to get …

The effect of dual cavity locations with strut injection configuration in a supersonic flow under
reacting conditions has been numerically evaluated. The simulation is performed by …