Scramjet is a promising propulsion technology that provides efficient and flexible access-to-
space and high-speed point-to-point transportation. Since the design process of scramjet …

Compared to pulse detonation engine and rotating detonation engine, oblique detonation
engine has the advantage of higher flight Mach number. However, it is still challenging to …

The interactions between oblique and bow shock waves are significant problems related to
the aerodynamic force and thermal performance of hypersonic vehicles, but few studies …

The viscosity effects on weak shock wave reflection are investigated with the Navier–Stokes
and DSMC flow solvers. It is shown that the viscosity plays a crucial role in the vicinity of …

Air intakes play a crucial role in the operation of scramjet engines, one of the most promising
hypersonic airbreathing propulsion technologies for efficient and flexible space …

For Mach reflection in steady supersonic flow, the slipline and reflected shock wave from the
triple point are disturbed by secondary Mach waves generated over the slipline and by the …

The asymmetrical Mach reflection configuration is studied analytically in this paper, using an
asymmetrical model extended from a recent symmetrical model and accounting for the new …

This paper presents a vortex breakdown study due to the interaction between a Batchelor
vortex and the crossing of oblique shock waves with Mach numbers of 3.5 and 5.0 …

In this work we study the open channel flow through a linear contraction. We focus on the
flow configuration with a two-dimensional jump in the contraction discussed by Akers and …

In this Letter, the dynamic effect of rotation on unsteady shock interaction between an
oblique shock wave and bow shock ahead of an elliptic cylinder is numerically investigated …