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Study of limits to the rotation function in the SA-RC turbulence model 被引量:1

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摘要 The Rotation and Curvature(RC)correction is an important turbulence model modifi-cation approach,and the Spalart-Allmaras model with the RC correction(SA-RC)has been exten-sively studied and used.As a multiplier of the modelling equation’s production term,the rotation function f_(r1)should have a cautiously designed value range,but its limit varies in different models and flow solvers.Therefore,the need of restriction is discussed theoretically,and the common range of f_(r1)is explored in Burgers vortexes.Afterwards,the SA-RC model with different limits is tested numerically.Negative f_(r1)always appears in the SA-RC model,and the difference between simula-tion results brought by the limits is not negligible.A lower limit of 0 enhances turbulence produc-tion,and therefore the vortex structures are dissipated faster and shrink in size,while an upper limit plays an opposite role.Considering that the lower limit of 0 usually promotes the simulation accu-racy and fixes the numerical defect,whereas the upper limit worsens the predictive performance in most cases,it is recommended to limit f_(r1)non-negative while utilizing the SA-RC model.In addi-tion,the RC-corrected model has a better prediction of the attached flow near curved walls,while the SA-Helicity model largely improves the simulation accuracy of three-dimensional large-scale vortices.The model combining both corrections has the potential to become more adaptive and more accurate.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2023年第1期246-265,共20页 中国航空学报(英文版)
基金 supported by the National Natural Science Foundation of China(Nos.51976006,51790513) the Aeronautical Science Foundation of China(No.2018ZB51013) the National Science and Technology Major Project,China(2017-II-003-0015) the Open Fund from State Key Laboratory of Aerodynamics,China(No.SKLA2019A0101).
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