Review of Unsteady Vortex Flows over Slender Delta Wings

By I. Gursul. 2005

222 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/ef46dc390f6cb7c602075510a20bbb2e44905942

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. Zhijin Wang
2. I. Gursul
3. Miguel R. Visbal
4. R. Gordnier
5. Eleni Vardaki
6. D. Rizzetta
7. Pinunta Rojratsirikul
8. Wei Shyy

In Computational Mechanics

1. Zhijin Wang
2. I. Gursul
3. Miguel R. Visbal
4. R. Gordnier
5. Eleni Vardaki
6. Christophe Bogey
7. Christophe Bailly
8. Wei Shyy

Citations in the corpus

• Unsteady aerodynamics of nonslender delta wings (2005, background): “Note that this range of natural frequencies of shear layer is much lower than those for slender wings [21, 24].”
• Review of flow control mechanisms of leading-edge vortices (2006, background): “Experiments and theoretical explanations of the vortex breakdown phenomenon [3] agree that there are two important parameters affecting the occurrence and movement of vortex breakdown: swirl level and pressure gradient.”