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The DES analysis of strong compressibility flow, LES mode is intentionally performed in boundary layer with the conventional empirical constant value of 0.65. In this study, an expression is suggested to determine the value dynamically by using a distribution function of the ratio of turbulence length scale and wall distance which is used in S-A DDES model for RANS mode protection. The application of the dynamic presents better prediction than previous results those used constant but different values.

Dynamic Correction of DES Model Constant for the Advanced Prediction of Supersonic Base Flow