Progress with verification and stabilization of Reynolds stress models using the CFD Software by ONERA, DLR, Airbus (CODA)

Kurzfassung

The current work targets verification of the SSG/LRR RSM model in CODA with 3D test cases like the transonic flow around the ONERA M6 wing, the DLR-F23 and the transonic drag-prediction workshop (DPW) CRM case using reference results from the DLR TAU code and CFL3D. We also describe several challenges encountered while performing these verification tests. Some strategies were attempted to navigate the difficulties and the ongoing efforts are focused to gain a better understanding from the experience.