Systematic studies on separation induced low-frequency unsteadiness in a canonical
supersonic combustor are implemented through wind tunnel experiment and numerical …

A delayed detached eddy simulation of an overexpanded nozzle flow with shock-induced
separation is carried out at a Reynolds number of (non-symmetric) pressure mode and is …

A three-dimensional high-fidelity numerical simulation of a small-scale solid rocket motor is
carried out adopting the implicit large-eddy simulation (ILES) approach to investigate the …

Shock-induced flow separation in an overexpanded supersonic planar nozzle is
investigated numerically by means of three-dimensional wall-modeled large-eddy …

Supersonic ejectors are passive gasdynamic devices that compress a low-pressure fluid by
utilizing the kinetic energy of a high-pressure fluid in a variable area duct. The ejector …

Rocket nozzles accelerate combustion products or high pressure gases to
supersonic/hypersonic velocities. The planar nozzles have rectangular cross-sections. At …

Unsteady side loads observed in supersonic nozzles operating in over-expanded regimes
are most often associated with intrinsic unsteadiness of the shock system and separation …

Abstract Large Eddy Simulations (LES) of an over-expanded conical nozzle are performed
to study the complex interaction between the turbulent boundary layer, the internal shock …

To overcome the lack of resolved turbulent flow structures generated by the improved
delayed detached eddy simulation (IDDES) model when simulating the shock wave and …

This Paper is a computational investigation of a scramjet nozzle design based on maximum
thrust theory and its feasibility analysis. A new design method for a two-dimensional …