The Effect of Wing-Tip Vortices on the Flow Around a NACA0012 Wing

Toosi S, Peplinski A, Schlatter P, Vinuesa R (2024)

Publication Type: Book chapter / Article in edited volumes

Publication year: 2024

Publisher: Springer Science and Business Media B.V.

Series: ERCOFTAC Series

Book Volume: 31

Pages Range: 183-188

DOI: 10.1007/978-3-031-47028-8_28

Abstract

The wing-tip vortices are formed near the tip of finite-span, lift-generating surfaces as a result of the pressure difference between the pressure and suction sides of the wing.

Involved external institutions

Royal Institute of Technology / Kungliga Tekniska Högskolan (KTH) SE Sweden (SE)

How to cite

APA:

Toosi, S., Peplinski, A., Schlatter, P., & Vinuesa, R. (2024). The Effect of Wing-Tip Vortices on the Flow Around a NACA0012 Wing. In (pp. 183-188). Springer Science and Business Media B.V..

MLA:

Toosi, S., et al. "The Effect of Wing-Tip Vortices on the Flow Around a NACA0012 Wing." Springer Science and Business Media B.V., 2024. 183-188.

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