Numerical analysis of a scramjet combustor with different cavity flame holders has been
carried out using ANSYS 16-FLUENT tool. In this research article the internal fluid flow …

Supersonic combustion was experimentally investigated in a strut-cavity based scramjet
combustor with kerosene and pilot hydrogen as fuels. Strut-cavity is the space between two …

Cavities have been extensively studied as flame holding devices for scramjets. Wall cavities
are known to have issues of fuel nonuniformity and flame close to the wall. Although strut …

A study on flow dynamics in strut cavity and wall cavity in different freestream Mach numbers
using numerical simulations has been conducted. A strut cavity is the space between two …

The effect of Tandem-Hole configuration on penetration and combustion in supersonic
crossflow was studied using three injectors having two tandem holes of 0.7 mm diameter …

In this study, the supersonic flow over strut cavities was experimentally studied to
understand flow features. Instantaneous schlieren imaging in non-reacting flow experiments …

Flow around the open strut cavity has been investigated numerically. Open strut cavity is the
cavity between two struts placed in tandem, along the flow. The simulation is done for the …