The flow field in a two-dimensional three-ramp hypersonic mixed-compression inlet in a
freestream Mach number of M∞= 5 is numerically solved to understand the unsteady …

The isolator plays a major role in the scramjet engine by providing suitable pressure for the
combustion process. It is situated between the inlet and the combustion chamber. The …

The nature of flow field inside the scramjet engine consists of shock-shock interaction and
the shock boundary layer interaction. For a sustained combustion, a device called isolator …

The isolator plays a critical role in the scramjet engine situated between the inlet and the
combustion chamber. The flow field is more complex with shock–shock interaction and …

The mixed compression scramjet engine intake was numerically simulated to study the
characteristic of shock wave induced boundary layer separation leading to the formation of …

The effects of back pressure and cavity L/D ratio on the shock wave structure in the cold flow
field of a typical cavity-based scramjet combustor with combined inlet and isolator is …

An isolator is a device that connects the inlet and combustion chambers of RAMJET or
SCRAMJET engines. The isolator will slow down the flow and increase static pressure with …

The dual mode engine is operated in scramjet mode in hypersonic flow and in ramjet mode
in supersonic flow. Numerical simulation is carried out using ANSYS Fluent to study …