Linear analysis of the cylinder wake mean flow
By Dwight Barkley. 2006
385 citations recorded by the source corpus.
Subfields: Computational Mechanics, Environmental Engineering
View Paper: https://www.semanticscholar.org/paper/93d48a9b846d8bd9ef92e4b597521e3cec809432
How researchers see this paper
The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.
In Computational Mechanics
- Clarence W. Rowley
- Denis Sipp
- Steven L. Brunton
- Dan S. Henningson
- A. Barbagallo
- Peter J. Schmid
- Shervin Bagheri
- O. Marquet
In Environmental Engineering
- Philipp Schlatter
- Denis Sipp
- Clément Mettot
- F. Sartor
- Dan S. Henningson
- Shervin Bagheri
- P. Meliga
- Weiwei Zhang
Citations in the corpus
- Mechanism of frequency lock-in in vortex-induced vibrations at low Reynolds numbers (2015, positive): “For Re= 60, the eigenfrequency of the uncoupled WM analysed by our unsteady aerodynamic model is Fw−l = 0.12, which is consistent with that obtained by Barkley (2006) from linear stability analysis of the base flow.”
- Dynamics and Control of Global Instabilities in Open-Flows: A Linearized Approach (2010, background): “The hydrodynamic stability community [36] has incorporated these new tools into the stability analyses of increasingly complex configurations, among them: Barkley et al. [37] for the case of a backward-facing step; Gallaire et al. [38] for the flow over a smooth bump; Sipp et al. [11] for the flow o”
- Global stability of a jet in crossflow (2009, background): “Similar to observations of the wake behind a cylinder (Barkley 2006), the steady separation region (downstream of the jet exit) is altered due to the saturated global modes yielding a significantly larger separation bubble and mean flow distortion.”
- Stability, Receptivity, and Sensitivity Analyses of Buffeting Transonic Flow over a Profile (2015, background): “Such results are not common: for example, in the case of cylinder flow [34], the base-flow and limit-cycle frequencies increasingly diverge as the Reynolds number departs from criticality.”
- Coherent structures in a swirl injector at Re = 4800 by nonlinear simulations and linear global modes (2016, methodology): “(2003) states that a stability analysis around a mean flow will produce the limit cycle as a neutrally stable global mode, which was later confirmed by Barkley (2006) for the cylinder flow.”
- Stability and receptivity characteristics of a laminar separation bubble on an aerofoil (2010, background): “This trend agrees with the work of Barkley (2006), who, for the case of bluff-body shedding, determined that stability analysis of the timeaveraged flow exhibits reduced growth rates as compared with that of a symmetrized ‘base flow’.”
- Feedback control of unstable steady states of flow past a flat plate using reduced-order estimators (2009, methodology): “These modes are qualitatively similar to the structures during periodic vortex shedding, but have different spatial wavelengths, as reported in earlier studies by Noack et al. (2003) and Barkley (2006).”
- Global stability of base and mean flows: a general approach and its applications to cylinder and open cavity flows (2007, methodology): “In the case of the cylinder flow, several authors, including Ding & Kawahara (1999), Barkley (2006) and Giannetti & Luchini (2007), revisited the linear stability of this flow recently.”
- Conditions for validity of mean flow stability analysis (2016, neutral): “For example, in the cylinder case, a linear stability analysis around the mean flow gives an excellent prediction of the vortex shedding frequency, even far from criticality (Pier 2002; Barkley 2006).”
- Sensitivity analysis and passive control of cylinder flow (2008, background): “Note that the global stability analysis of the base flow fails to capture the frequency of the vortex shedding for Reynolds numbers above Rec (for further details, see Barkley 2006; Sipp & Lebedev 2007).”