The prediction of unstart boundaries of hypersonic inlets is significant to the engine control.
To correct the previous conclusions based on the one-dimensional and inviscid flow …

A cooling film (Mach 2.3) is injected into a supersonic wind tunnel's (Mach 3.8) flow field. As
the curvature radius decreases, mixing layer destabilization is delayed on the CV (convex …

Predicting the transient flow fields that develop when a shock wave passes through an area
expansion is a fundamental problem in compressible fluid mechanics and significant in …

The development of shock tubes and understanding of shock wave propagation and its
interaction with a model is of significant interest in various domains. In this context, shock …

Curvature plays a crucial role in evolving supersonic cooling film flow-field structures. Flow-
field structural images were captured using nanotracer-based planar laser scattering,, and …

Curvature plays a pivotal role in the evolution of supersonic boundary layer flows. Under the
inflow condition of Ma= 3.8, the influence of curvature on the flow over a backward-facing …

Regular reflection to Mach reflection (RR–MR) transition in short wedges Page 1 J. Fluid
Mech. (2024), vol. 998, A38, doi:10.1017/jfm.2024.826 Regular reflection to Mach reflection (RR–MR) …

Rotating detonation engines (RDEs) have been marked as the so-called holy grail of
propulsion and power generation systems, working through detonation of fuel and oxidiser …

The objective of the present study is to understand the behavior of a normal shock wave,
generated using a shock tube, traveling on a double concave ramp with a radius of …

When a moving shock wave reflects from a concave cylindrical surface, transition from an
Inverse Mach Reflection (InMR) to a Transitioned Regular Reflection (TRR) takes place. The …