20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2015
DOI: 10.2514/6.2015-3637
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Development of a Two-Temperature Open-Source CFD Model for Hypersonic Reacting Flows

Abstract: This version is available at https://strathprints.strath.ac.uk/55053/ Strathprints is designed to allow users to access the research output of the University of Strathclyde. Unless otherwise explicitly stated on the manuscript, Copyright © and Moral Rights for the papers on this site are retained by the individual authors and/or other copyright owners. Please check the manuscript for details of any other licences that may have been applied. You may not engage in further distribution of the material for any pro… Show more

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Cited by 10 publications
(6 citation statements)
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“…Figure 3 (right) plots the pressure distributions versus time. The solid lines are results from this work and the circle points are reference results from [20]. Good agreement is found for all the results.…”
Section: A Zero-dimensional Cubesupporting
confidence: 55%
“…Figure 3 (right) plots the pressure distributions versus time. The solid lines are results from this work and the circle points are reference results from [20]. Good agreement is found for all the results.…”
Section: A Zero-dimensional Cubesupporting
confidence: 55%
“…The hy2Foam solver has already been validated by considering the thermal relaxation of a single-species gas [44]. Since new features have been added such as corrected species-dependent coefficients in the interspecies relaxation time (Park 1993, Ref.…”
Section: Vibrational-translational Relaxation Of a Single-species Gasmentioning
confidence: 99%
“…hy2Foam is a fusion of additional physical models to incorporate thermochemical nonequilibrium with the existing solver called rhoCentralFoam, developed for compressible flows and based on the OpenFOAM framework [16]. The thermochemical nonequilibrium modelling of the solver was validated for several cases ranging from zero-dimensional chemical kinetics to multidimensional hypersonic flows [9,[17][18][19], and the Energies 2020, 13, 606 4 of 17 underlying numerics of the solver was also validated for the hypersonic cases relevant to the present study [20][21][22].…”
Section: Methodsmentioning
confidence: 99%