2022
DOI: 10.1016/j.ijheatfluidflow.2022.109047
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Sparse Bayesian Learning of Explicit Algebraic Reynolds-Stress models for turbulent separated flows

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Cited by 13 publications
(5 citation statements)
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“…3. One specific turbulence closure methodology that has received much attention is the algebraic Reynolds stress model (ARSM), where data-driven techniques are used to improve coefficient determination in the tensor representation of constitutive relations [50][51][52][53][54][55][56]. 4.…”
Section: Machine-learning and Ransmentioning
confidence: 99%
“…3. One specific turbulence closure methodology that has received much attention is the algebraic Reynolds stress model (ARSM), where data-driven techniques are used to improve coefficient determination in the tensor representation of constitutive relations [50][51][52][53][54][55][56]. 4.…”
Section: Machine-learning and Ransmentioning
confidence: 99%
“…These models, formulated as tensor polynomials, were inferred from high-fidelity data and allowed for a cost-effective correction of the k-ω SST model. Additionally, the works of Huijing et al [42], Zhang et al [43], Cherroud et al [44] have been instrumental in the further promotion and enhancement of SpaRTA.…”
Section: Introductionmentioning
confidence: 99%
“…These results suggest that the use of wall models cannot predict the impending boundary layer detachment when using the k − ω SST model. Simultaneously, k − ω SST is known to overestimate boundary layer separation and re-attachment by the literature [86,87]. Future work suggests performing high-fidelity numerical simulations and/or experimentally investigating these regions to validate the results and which methodology is more accurate.…”
Section: V3 Resultsmentioning
confidence: 95%
“…There are, however, slight deviations in the mean value of the numerical prediction seen at x = 1D. These deviations suggest a slight underprediction of the axial velocity at the centre and top sections of the pipe and could indicate that the CFD methodology underestimates the turbulence diffusion in some regions of the flow as well as boundary-layer detachment and reattachment [29,86,87]. Nevertheless, all numerical results are confined inside experimental uncertainty bounds of 2σ in the analysed profiles, where the slight disagreement of high Re cases is expected due to their added physical complexity and the prediction of turbulent fields.…”
Section: Iii32 Experimental Validation Of Axial Velocitymentioning
confidence: 99%
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