Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
1718314 | Aerospace Science and Technology | 2013 | 10 Pages |
Abstract
The numerical simulation of the flow around a 65° delta wing configuration with rounded leading edges is presented. For the numerical simulation the DLR TAU-Code is used which is based on an unstructured hybrid mesh approach. Within this paper several numerical results are shown, solving the steady RANS equations by different turbulence models. The simulations are carried out within the RTO/AVT-113 task group focusing on experimental and numerical research on delta wing configurations with rounded leading edges. Within this paper the focus is related to the flow topology depending on the angle of attack as well as on Reynolds number effects. Finally the results are compared and verified by experimental data.
Related Topics
Physical Sciences and Engineering
Engineering
Aerospace Engineering
Authors
Andreas Schütte, Heinrich Lüdeke,