An analysis of the correlations between the turbulent flow and the sound pressure fields of subsonic jets

By Christophe Bogey, Christophe Bailly. Journal of Fluid Mechanics, 2007

200 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics, Environmental Engineering

View Paper: https://www.semanticscholar.org/paper/d0b3ea17d87c26e6965422415971df1f97d15f8d

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. P. Jordan
3. Christophe Bogey
4. Christophe Bailly
5. André V. G. Cavalieri
6. Nicolas de Cacqueray
7. Y. Gervais
8. Olivier Marsden

In Computational Mechanics

1. Tim Colonius
2. P. Jordan
3. Christophe Bogey
4. Christophe Bailly
5. André V. G. Cavalieri
6. Nicolas de Cacqueray
7. Olivier Marsden
8. Y. Gervais

In Environmental Engineering

1. Tim Colonius
2. P. Jordan
3. André V. G. Cavalieri
4. Christophe Bogey
5. Christophe Bailly
6. Y. Gervais
7. Olivier Marsden
8. Daniel Rodríguez

Citations in the corpus

• Influence of nozzle-exit boundary-layer conditions on the flow and acoustic fields of initially laminar jets (2010, methodology): “In this case, the source responsible for the downstream noise component, associated with the mixing-layer merging on the centreline at the end of the jet core in Bogey & Bailly (2007), is then strengthened by the pairings.”
• Wavepackets in the velocity field of turbulent jets (2012, methodology): “…point in the velocity field and a single microphone, as often done in the literature (Lee & Ribner 1972; Schaffar 1979; Juvé, Sunyach & Comte-Bellot 1980; Panda, Seasholtz & Elam 2005; Bogey & Bailly 2007); the second was between a given azimuthal mode in both the velocity and the acoustic field.”
• Influence of initial turbulence level on the flow and sound fields of a subsonic jet at a diameter-based Reynolds number of 105 (2012, methodology): “…also be found to be significant on the centreline, which was attributed to the formation and evolution of ring vortices in the shear layers in Camussi & Guj (1999), and to the merging of turbulent structures at the end of the potential core in Bogey et al. (2003, 2009a,b) and Bogey & Bailly (2007).”
• A shock-capturing methodology based on adaptative spatial filtering for high-order non-linear computations (2009, methodology): “These methods have been successfully implemented in previous studies to perform direct noise computations for configurations such as subsonic and supersonic jets [12,52,53], and flows around an airfoil [54].”
• Wave Packets and Turbulent Jet Noise (2013, background): “In this pursuit, one wishes to go beyond two-point flow-acoustic correlations (Bogey & Bailly 2007, Juvé et al. 1980, Lee & Ribner 1972, Panda et al. 2005, Seiner & Reethof 1974, Tam et al. 2008), which provide limited insight because wave-packet structures are spatially extensive.”
• Turbulence and energy budget in a self-preserving round jet: direct evaluation using large eddy simulation (2009, background): “Bogey & Bailly (2006a,c, 2007) and Berland, Bogey & Bailly (2007) also investigated the initial flow development and noise generation in subsonic and supersonic jets.”