On self-sustained oscillations in two-dimensional compressible flow over rectangular cavities

By Clarence W. Rowley, Tim Colonius, A. Basu. Journal of Fluid Mechanics, 2002

528 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/a8e5ff8f226106eefdddcd5196d96a0f5e177d98

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. Tim Colonius
2. G. Brès
3. Sanjiva K. Lele
4. Steven L. Brunton
5. Clarence W. Rowley
6. G. Constantinescu
7. Seung-O Park
8. Kyoungsik Chang

In Computational Mechanics

1. Tim Colonius
2. Steven L. Brunton
3. G. Brès
4. Denis Sipp
5. Clarence W. Rowley
6. A. Barbagallo
7. J. Nathan Kutz
8. Sanjiva K. Lele

Citations in the corpus

• Constrained sparse Galerkin regression (2016, background): “Note that for compressible shear-driven cavity flows, a similar unstable feedback loop exists wherein the feedback mechanism is provided by upstream-propagating acoustic waves (Rossiter, 1964; Rowley et al., 2002; Yamouni et al., 2013).”
• Three-dimensional instabilities in compressible flow over open cavities (2008, methodology): “Other experimental (e.g. Gharib & Roshko 1987) and numerical (e.g. Rowley et al. 2002) studies on open cavity flows also report that larger shear-layer spreading rates are obtained as L/θ0 is increased, and ultimately lead to a higher dominant mode.”
• Dynamics and Control of Global Instabilities in Open-Flows: A Linearized Approach (2010, background): “Cavity flows, like those observed over bomb bays, are the site of violent unsteadiness related to powerful sound pressure waves that can cause severe structural vibrations [7].”
• Large-eddy simulation of a compressible flow in a three-dimensional open cavity at high Reynolds number (2004, background): “Such behaviour seems to be preferentially related to two-dimensional or axisymmetrical configurations and, according to Rowley et al. (2002), could be partially due to an absolute instability.”
• The mixing layer over a deep cavity at high-subsonic speed (2003, background): “The transition between the ‘shear layer mode’ and the ‘wake mode’ depends on the ratio L/θ0 (Gharib & Roshko 1987) and also on the Mach and Reynolds numbers (Rowley et al. 2002).”
• Computational aeroacoustics: progress on nonlinear problems of sound generation (2004, methodology): “DNS/LES with acoustic analogy . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 355 3.2.2.”
• Viscous linear stability analysis of rectangular duct and cavity flows (2004, background): “Taking c = −2 in (2.1) and scaling the result with the value of ¯ w at the midpoint of the integration domain, the Poisson problem may be solved in series form ( Rosenhead 1963 )”
• Model reduction for compressible flows using POD and Galerkin projection (2004, methodology): “The fully compressible Navier–Stokes equations were solved using sixth-order compact finite differences in space and fourth-order Runge–Kutta in time, resulting in a scheme with very low dispersion and dissipation, necessary to resolve acoustic waves.”
• Analysis of the flow and mass transfer processes for the incompressible flow past an open cavity with a laminar and a fully turbulent incoming boundary layer (2006, methodology): “The averaged rate of dδω/dx (x < 1.7) is 0.07 which is close to those obtained by Rowley et al. (2002) in their two-dimensional DNS compressible flow simulations with an incoming laminar boundary layer.”