Numerical investigations on the VFE-2 65-degree rounded leading edge delta wing using the unstructured DLR TAU-Code

You are here: Homepage > Search

Numerical investigations on the VFE-2 65-degree rounded leading edge delta wing using the unstructured DLR TAU-Code

Numerical investigations on the VFE-2 65-degree rounded leading edge delta wing using the unstructured DLR TAU-Code

Schütte, Andreas / Lüdeke, Heinrich

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.

Access

Check availability in my library

Order at Subito €

Export, share and cite

Document information

Title :

Numerical investigations on the VFE-2 65-degree rounded leading edge delta wing using the unstructured DLR TAU-Code

Contributors:

Schütte, Andreas (author) / Lüdeke, Heinrich (author)

Published in:

Aerospace Science and Technology ; 24 , 1 ; 56-65

Publication date :

2012-01-01

Size :

10 pages

ISSN :

DOI :

https://doi.org/10.1016/j.ast.2012.03.002

Type of media :

Article (Journal)

Type of material :

Electronic Resource

Language :

English

Keywords :

Vortical flow , Delta wing , Blunt leading edge , Experiments , Numerics , CFD , DES , RTO , VFE-2 , AVT , TAU-Code , DLR

Similar titles

Numerical investigations on the VFE 2 65-Degree rounded leading edge delta wing using the unstructured DLR-TAU-Code

Schuette, Andreas / Luedeke, Heinrich | AIAA | 2008

Numerical investigations on the VFE-2 65-degree rounded leading edge delta wing using the unstructured DLR TAU-Code

Schütte, Andreas | Online Contents | 2013

Numerical investigations on the VFE 2 65-Degree rounded leading edge delta wing using the unstructured DLR-TAU-Code

Schuette, A. / Luedeke, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008

Experiments on a 60-Degree Delta Wing with Rounded Leading-Edge Vortex Flaps

Kenichi Rinoie | AIAA | 2000

Flow Field Around Thick Delta Wing with Rounded Leading Edge

Yasuhara, Michiru / Nakamura, Yoshiaki / Nakajima, Yoshiji et al. | SAE Technical Papers | 1991

Access

Check availability in my library

Order at Subito €

Page navigation

Document information

Export, share and cite