2021
DOI: 10.1016/j.compfluid.2021.104994
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Numerical workflow for scale-resolving computations of space launcher afterbody flows with and without jets

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Cited by 5 publications
(13 citation statements)
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“…In order to contribute to the development of advanced numerical methods for bi-species supersonic mixing layers, two bi-species ZDES [22] computations are performed in this study on a well-known supersonic coaxial jets experiment run by Cutler et al [27,1] and reproduced numerically by several authors in the past with RANS [1,18] or RANS/LES formulations [17,23,19,21]. To meet the numerical challenges described above, the computations are run with an original hybrid numerical scheme [28] based on Ducros's sensor [29] associated to a low dissipation version of the AUSM scheme [30,31]. This new scheme is able to switch automatically from a low-dissipation formulation in presence of vortical structures to a more robust formulation in presence of shock waves (see Sec.…”
Section: Review Of Turbulent Mass Diffusion Modelling Techniquesmentioning
confidence: 99%
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“…In order to contribute to the development of advanced numerical methods for bi-species supersonic mixing layers, two bi-species ZDES [22] computations are performed in this study on a well-known supersonic coaxial jets experiment run by Cutler et al [27,1] and reproduced numerically by several authors in the past with RANS [1,18] or RANS/LES formulations [17,23,19,21]. To meet the numerical challenges described above, the computations are run with an original hybrid numerical scheme [28] based on Ducros's sensor [29] associated to a low dissipation version of the AUSM scheme [30,31]. This new scheme is able to switch automatically from a low-dissipation formulation in presence of vortical structures to a more robust formulation in presence of shock waves (see Sec.…”
Section: Review Of Turbulent Mass Diffusion Modelling Techniquesmentioning
confidence: 99%
“…In order to test different numerical strategies, we have adapted three mono-species schemes to bi-species flow: the AUSM+ [30], a robust upwind scheme, an adapted low-dissipative AUSM+(P) [31] (called here AUSM+(P) L-D) and a hybrid shock-capturing scheme combining the two previous AUSM type schemes to perform high-fidelity, scale-resolving simulations of compressible flows [28].…”
Section: Explicit Convective Fluxesmentioning
confidence: 99%
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