Numerical investigations on the VFE 2 65-Degree rounded leading edge delta wing using the unstructured DLR-TAU-Code-Reference-Cited by-同舟云学术

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

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Schuette Andreas¹,Luedeke Heinrich²

Affiliation:

1. German Aerospace Center

2. German Aeropspace Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-398

Reference20 articles.

1. Wagner, B.; Hitzel, S.; Schmatz, M.A.; Schwarz, W.; Hilgenstock, A.; Scherr, S.: Status of CFD validation on the vortex flow experiment. AGARD-CP437 (1988), Vol.1, pp.10-1to 10-10.

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2. Numerical Assessment of Leading- and Trailing-Edge Control on a Swept Lambda Wing;Journal of Aircraft;2018-03

3. What was learned from the new VFE-2 experiments;Aerospace Science and Technology;2013-01

4. Numerical simulation of the peculiar subsonic flow-field about the VFE-2 delta wing with rounded leading edge;Aerospace Science and Technology;2013-01

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