Flutter and limit cycle oscillations of two-dimensional panels in three-dimensional axial flow

By D. Tang, H. Yamamoto, Earl H. Dowell. 2003

179 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Control and Systems Engineering

View Paper: https://www.semanticscholar.org/paper/a2e18519f98cd5df79b2ec878ac29df15f4553d9

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. Earl H. Dowell
2. C. Souilliez
3. Lionel Schouveiler
4. Christophe Eloy
5. R. Lagrange
6. Michael J. Shelley
7. Jun Zhang

In Computational Mechanics

1. Earl H. Dowell
2. Brian P. Mann
3. Jinwu Xiang
4. C. Souilliez
5. Lionel Schouveiler
6. Christophe Eloy
7. R. Lagrange
8. Daochun Li

In Control and Systems Engineering

1. Brian P. Mann
2. Jinwu Xiang
3. C. Souilliez
4. Lionel Schouveiler
5. Christophe Eloy
6. R. Lagrange
7. Daochun Li
8. Yining Wu

Citations in the corpus

• Flapping dynamics of an inverted flag (2013, unknown): “(2013), vol. 736, R1, doi:10.1017/jfm.2013.555”
• Energy harvesting by means of flow-induced vibrations on aerospace vehicles (2016, background): “This configuration has been extensively investigated for its rich and complex dynamics [21-25].”
• Power extraction from aeroelastic limit cycle oscillations (2011, methodology): “The analyses in Tang et al. (2003) and Stanton and Mann (in review) detail two valid ways to approach this derivation that yield similar results.”
• Aeroelastic instability of cantilevered flexible plates in uniform flow (2008, methodology): “The nature of the bifurcation in this flutter instability has also been studied using a nonlinear beam equation for the plate and two-dimensional (Tang & Päıdoussis 2007) or three-dimensional (Tang et al. 2003) vortex methods to model the potential flow.”