Organized Oscillations of Initially-Turbulent Flow Past a Cavity
By J. Lin, Donald Rockwell. 2002
147 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/1127e3d379cedb05b497dde7898a8d41c053f0f3
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In Aerospace Engineering
In Computational Mechanics
- Pierre Sagaut
- L. Larchevêque
- T. Lê
- P. Comte
- Seung-O Park
- Kyoungsik Chang
- G. Constantinescu
- Sébastien Deck
Citations in the corpus
- 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): “Lin & Rockwell (2001) used particle image velocimetry (PIV) techniques to study the flow over a two-dimensional cavity (ReD ∼ 27 800) with a turbulent boundary layer inflow (momentum thickness was θ ∼ 0.049D).”
- Direct computation of the noise radiated by a subsonic cavity flow and application of integral methods (2003, unknown): “The present distributions can be compared to those obtained by Ziada and Rockwell [30] for the interaction between a shear layer and a wedge.”
- Large-eddy simulation of a compressible flow in a three-dimensional open cavity at high Reynolds number (2004, background): “They could be related to a modulation of the Rossiter modes by large-scale flow structures; see for instance Lin & Rockwell (2001) for an example of such a modulation.”