- Conference Article
14
- 10.2514/6.2006-717
Assessment of Numerical Methods for DNS of Shockwave/Turbulent Boundary Layer Interaction
- Jan 09, 2006
- 44th AIAA Aerospace Sciences Meeting and Exhibit
- Minwei Wu + 1 more +1
Various candidate sources of error for the discrepancy between previous direct numerical simulation (DNS) results of Wu et al. and experimental data of Bookey et al. are investigated. Deficiencies of current numerical methods for DNS of shockwave/turbulent boundary layer interactions (STBLI) are found. The weighted-essentially-non-oscillatory (WENO) method is improved by adding limiters in the smoothness measurement. In turn, the numerical dissipation is significantly reduced. For the compression ramp case, using the limiter results in increased size of the separation bubble and improved mean wallpressure distribution. In addition, a fourth-order low-dissipation Runge-Kutta method is found to give less dissipation than the typically used third-order low-storage Runge-Kutta method. Combining the limiter with the low-dissipation Runge-Kutta method gives better results. Good agreement is found for the size of the separation bubble and the wall-pressure distribution when comparing against the experimental data at the same conditions.
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