Speaker
Dr
Bodo Reimann
(German Aerospace Center (DLR))
Description
The DLR results of the ATD3 test case 2022 will be presented. The interaction of a free-flying ring with a two-dimensional curved shock wave has been simulated using the DLR TAU code. The flow solver was coupled with a 6-DoF motion module, dynamic grid adaptation has been used to capture the shock waves. A comparison between the numerical results and the experimental test case data will be presented and discussed.
Primary author
Dr
Bodo Reimann
(German Aerospace Center (DLR))
