Optimized Ristorcelli’s Compressibility Correction to the kω-SST Turbulence Model for Base Flow Analysis

초록

Compressibility correction methods to two-equation turbulence models have been used widely to account for the compressibility effects in turbulent high-speed flows. The present study aims at improving the accuracy of base pressure/drag predictions with the two-equation turbulence models. To this end, a simplified Ristorcelli’s compressibility correction is selected to perform computational analysis for base flows in conjunction with the k − ω SST turbulence model. The source terms arise in the ω equation when Ristorcelli’s correction model is applied to the k − ω turbulence model. Further improvement is sought by applying Bayesian optimization to determine a user-defined parameter in Ristorcelli’s correction model. Numerical analyses have been conducted for flows past axisymmetric bases and projectiles, and the validity of the optimized correction model is examined. The solutions with and without the optimized correction are presented and compared with the results of the standard k − ω SST turbulence model and the experimental data.

출판유형
발행기관
International Journal of Aeronautical and Space Sciences
박진석
박진석
조교수

공기역학, 전산유체역학, 고성능 컴퓨팅을 연구하고 있습니다.