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|Title:||Computation of turbulent separated nozzle flow by a lag model||Authors:||Xiao, Q.
|Issue Date:||Mar-2005||Citation:||Xiao, Q.,Tsai, H.-M.,Liu, F. (2005-03). Computation of turbulent separated nozzle flow by a lag model. Journal of Propulsion and Power 21 (2) : 368-371. ScholarBank@NUS Repository.||Abstract:||The capability of the lag model for shock-induced separated flows in supersonic nozzles was discussed. The Reynold-averaged Navier-Stokes equations and the baseline Wilcox k-ω turbulence model were used to predict the equilibrium eddy viscosity. It was found that the lag model introduced history effect and relaxation of the eddy viscosity over the equilibrium values predicted by the baseline model. Analysis shows that the inclusion of the lag model significantly improves the results where there is strong shock-induced separation.||Source Title:||Journal of Propulsion and Power||URI:||http://scholarbank.nus.edu.sg/handle/10635/116273||ISSN:||07484658|
|Appears in Collections:||Staff Publications|
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