Leading-Edge Vortex Structure of Nonslender Delta Wings at Low Reynolds Number

By M. Ol, Morteza Gharib. 2003

138 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/fb43b57f516c6fb98e4f3e93c0aea89f6e1b553d

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. I. Gursul
2. Miguel R. Visbal
3. R. Gordnier
4. James H. J. Buchholz
5. Craig J. Wojcik
6. Zhijin Wang
7. D. Rizzetta
8. Pinunta Rojratsirikul

In Computational Mechanics

1. I. Gursul
2. Miguel R. Visbal
3. R. Gordnier
4. James H. J. Buchholz
5. Craig J. Wojcik
6. Christophe Bogey
7. Christophe Bailly
8. Zhijin Wang

Citations in the corpus

• Unsteady aerodynamics of nonslender delta wings (2005, background): “The structure of vortex breakdown over a 50° sweep delta wing has been studied in greater detail both computationally [16] and by PIV measurements [11, 15, 30, 40].”
• Vorticity transport in the leading-edge vortex on a rotating blade (2014, background): “…classical problem of a vortex interacting with a wall (Doligalski, Smith & Walker 1994), and analogous development of the opposite-sign layer has also been observed under leading-edge vortices on delta wings (Lin & Rockwell 1995; Visbal & Gordnier 1995; Shih & Ding 1996, 2002; Ol & Gharib 2003).”