This paper presents HALO3D, a CFD code simulating the wide range of Mach numbers a
hypervelocity vehicle experiences. HALO3D is composed of (a) a RANS edge-based Finite …

Purpose This work aims to describe the physical and numerical modeling of a CFD solver for
hypersonic flows in thermo-chemical non-equilibrium. This paper is the second of a two-part …

In the context of the development of HALO3D (High Altitude Low Orbit 3D), an edge-based
Finite Element Method multidisciplinary solver for hypersonic flows, this paper presents the …

Purpose This paper aims to describe the physical and numerical modeling of a new
computational fluid dynamics solver for hypersonic flows in thermo-chemical non …

The paper presents an edge-based finite element method for the simulation of three-
dimensional hypersonic flows subject to an imposed magnetic field. Under the …

Numerical simulations of the effects of gas-surface interactions on gas composition and heat
flux at the surface are of paramount importance to the design of thermal protection system of …

The paper presents an edge-based finite element method formulation for the coupled
magnetohydrodynamic equations used for the simulation of magnetogasdynamic propulsion …

HALO3D (High-Altitude Low-Orbit, 3D) est un logiciel CFD développé par le Laboratoire
CFD de McGill pour simuler les écoulements chevauchant les basses vitesses de Mach …

The present work extends the capabilities of a compressible Navier-Stokes solver into a
thermo-chemical non-equilibrium hypersonic flow solver. Finite-rate chemistry and two …

2. Moderne hochauflösende bildgebende Verfahren wie Mikro-Computertomographie
(µCT), Magnetresonanztomographie (MRT), Ultraschall-und Rasterelektronenmikroskopie …