Eilmer: an open-source multi-physics hypersonic flow solver

NN Gibbons, KA Damm, PA Jacobs… - Computer Physics …, 2023 - Elsevier
This paper introduces Eilmer, a general-purpose open-source compressible flow solver
developed at the University of Queensland, designed to support research calculations in …

Thermo-chemical nonequilibrium effects on combustion characteristics of a transverse jet in the scramjet

J Zhang, Z Wang, C Liu, M Sun, H Wang, J Ai… - Aerospace Science and …, 2024 - Elsevier
As the Mach number increases, the local static temperature gradually approaches the
characteristic gas vibration/dissociation temperature, and significant thermo-chemical …

An open-source CFD solver for planetary entry

V Casseau - 2017 - stax.strath.ac.uk
Abstract hy2Foam is a newly-coded open-source two-temperature computational fluid
dynamics (CFD) solver that aims at (1) giving open-source access to a state-of-the-art …

Characterisation of the eddy dissipation model for the analysis of hydrogen-fuelled scramjets

J Hoste, M Fossati, IJ Taylor, RJ Gollan - The Aeronautical Journal, 2019 - cambridge.org
The eddy dissipation model (EDM) is analysed with respect to the ability to address the
turbulence–combustion interaction process inside hydrogen-fuelled scramjet engines …

Transient numerical simulation of hemispherical cone with combined opposing jet in hypersonic flow

W Zhang, X Wang, Z Zhang, T Su - Acta Astronautica, 2020 - Elsevier
A novel combined opposing (CBO) jet is proposed in this study, which consists of a circle
opposing (CO) jet and an annulus opposing (AO) jet. Three CBO jets with the internal …

Worst-Case Learning under a Multi-fidelity Model

S Foucart, N Hengartner - arXiv preprint arXiv:2406.14418, 2024 - arxiv.org
Inspired by multi-fidelity methods in computer simulations, this article introduces procedures
to design surrogates for the input/output relationship of a high-fidelity code. These …

Numerical analysis of thermochemical nonequilibrium flows in a model scramjet engine

S Han, S Lee, BJ Lee - Energies, 2020 - mdpi.com
This numerical study was conducted to investigate the flow properties in a model scramjet
configuration of the experiment in the T4 shock tunnel. In most numerical simulations of …

Development and Validation of a Compressible Reacting Gas-Dynamic Flow Solver for Supersonic Combustion

A Gilmanov, P Gokulakrishnan, MS Klassen - Dynamics, 2024 - mdpi.com
An approach based on the OpenFOAM library has been developed to solve a high-speed,
multicomponent mixture of a reacting, compressible flow. This work presents comprehensive …

Numerical investigation of the STRATOFLY MR3 propulsive nozzle during supersonic to hypersonic transition

L Nista, BH Saracoglu - AIAA Propulsion and Energy 2019 Forum, 2019 - arc.aiaa.org
T e demand for discovering new commercial routes as well as the possibility to shortening
long haul flights from intercontinental to antipodal trajectories boosted the interest of civil …

Modeling scramjet supersonic combustion via eddy dissipation model

JJOE Hoste, M Fossati, IJ Taylor… - 68th International …, 2017 - strathprints.strath.ac.uk
Scramjet technology has gained considerable interest in multi-stage to orbit design concepts
due to its reusability and high specific impulse at high-Mach regimes. The aim of the present …