Unsteady aerodynamics of nonslender delta wings

By I. Gursul, R. Gordnier, Miguel R. Visbal. 2005

337 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/cc3b5d8ba62789d5026080aff0fc908c2927de24

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. Eleni Vardaki
3. Pinunta Rojratsirikul
4. I. Gursul
5. Wei Shyy
6. Chang-kwon Kang
7. Hikaru Aono

In Computational Mechanics

1. Zhijin Wang
2. Eleni Vardaki
3. Pinunta Rojratsirikul
4. O. Bendiksen
5. I. Gursul
6. Wei Shyy
7. Chang-kwon Kang
8. Hikaru Aono

Citations in the corpus

• Unsteady fluid–structure interactions of membrane airfoils at low Reynolds numbers (2009, background): “It is possible that membrane vibrations can excite the separated shear layer forming the tip vortices and promote reattachment ( Gursul et al. 2005 ).”
• Review of flow control mechanisms of leading-edge vortices (2006, background): “typically Λ ≥ 65°, has been extensively studied and is now reasonably well understood, the flow over lower sweep wings has only recently attracted more attention [9].”
• Review of unsteady transonic aerodynamics: Theory and applications (2011, background): “Vortex-dominated unsteady transonic flows over highly swept delta or cranked delta wings representative of future supersonic transport designs have been difficult to predict (or even understand) based on calculations using current production RANS codes; see for example the data from the US High Spee”
• Three-dimensional flows around low-aspect-ratio flat-plate wings at low Reynolds numbers (2009, neutral): “compared to the ones from higher Reynolds number flow ( Gursul, Gordnier & Visbal 2005 ).”