Abstract Space debris that re-enter the Earth's atmosphere can be partially or fully ablated
along the trajectory path after hitting the atmosphere layers, once these become denser …

The separation process of multi-spheres in hypersonic flow has been experimentally
investigated. The experiments were conducted in a shock tunnel at a nominal freestream …

In this work, an overview of flow diagnosis in a shock tunnel is made by means of using
established techniques that are easy to setup, economical to arrange, and simple to …

The separation behavior of two bodies was experimentally investigated in a shock tunnel.
Simple-shaped bodies, including a cylinder, cube, and sphere, with a size of 3 or 5 mm were …

This paper describes a numerical investigation on the effects of wall temperature and
leading-edge bluntness on hypersonic laminar separation induced by a finite-span …

Hypersonic flow over a cylinder was modeled using the direct simulation Monte Carlo
method to study how nitric oxide (NO) Ultraviolet emission profiles are a test of high-fidelity …

This paper describes laminar hypersonic leading edge separation. Such a configuration of
separated flow was originally studied by Chapman et al.(NACA Tech. Rep. 1356, 1958) at …

A comprehensive study of the fundamental characteristics of leading-edge separation in
rarefied hypersonic flows is undertaken and its salient features are elucidated. Separation of …

The separation and shock wave formation on the aft-body of a hypersonic adiabatic circular
cylinder were studied numerically using the open source software OpenFOAM. The …

The paper presents a computational and an experimental investigation of base flow of a
circular cylinder at hypersonic speeds. Effects of chemistry and wall temperature on the flow …