2019
DOI: 10.1016/j.ces.2018.08.020
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A delayed detached eddy simulation model with low Reynolds number correction for transitional swirling flow in a multi-inlet vortex nanoprecipitation reactor

Abstract: The objective of the presented work is to verify a delayed detached eddy simulation (DDES) model for simulating transitional swirling flow in a micro-scale multi-inlet vortex reactor (MIVR). The DDES model is a k-w based turbulence model with a low Reynolds number correction applied to the standard k-w model such that the Reynolds-averaged Navier-Stokes (RANS) component of the DDES model is able to account for low Reynolds number flow. By limiting the dissipation rate in the k-equation, the large-eddy simulati… Show more

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Cited by 13 publications
(1 citation statement)
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“…Hence, using accurate models is critical for predicting the anisotropy and non-equilibrium effects. To date, the issues of CFD-based numerical simulation remain in the flow simulation process, including: (i) because of the complexity [12,13] it is necessary to determine the vortex flow characteristics and patterns; moreover, the global flow information is difficult to be measured precisely due to its small size (body diameter is around 6-100 mm); (ii) compared to large-scale vortex reactor/separators, extra lateral and normal divergence usually occurs, causing an increasing difficulty in numerical simulation [14]; (iii) for most investigations, however, the effect of transitional flow usually does not take into account in the simulation [15][16][17]; (iv) for SVR/Ss with variable designs and operating parameters, the generalizability of the numerical models has not been comprehensively evaluated based on techno-economic performances.…”
Section: Introductionmentioning
confidence: 99%
“…Hence, using accurate models is critical for predicting the anisotropy and non-equilibrium effects. To date, the issues of CFD-based numerical simulation remain in the flow simulation process, including: (i) because of the complexity [12,13] it is necessary to determine the vortex flow characteristics and patterns; moreover, the global flow information is difficult to be measured precisely due to its small size (body diameter is around 6-100 mm); (ii) compared to large-scale vortex reactor/separators, extra lateral and normal divergence usually occurs, causing an increasing difficulty in numerical simulation [14]; (iii) for most investigations, however, the effect of transitional flow usually does not take into account in the simulation [15][16][17]; (iv) for SVR/Ss with variable designs and operating parameters, the generalizability of the numerical models has not been comprehensively evaluated based on techno-economic performances.…”
Section: Introductionmentioning
confidence: 99%