Unstructured Large-Eddy Simulations of Supersonic Jets
By G. Brès, Frank E. Ham, Joseph W. Nichols, Sanjiva K. Lele. 2017
208 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics, Environmental Engineering
View Paper: https://www.semanticscholar.org/paper/9806b6af1909cffbfcc60fe1fe26ce1d27824072
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
- Oliver T. Schmidt
- Aaron Towne
- Tim Colonius
- P. Jordan
- André V. G. Cavalieri
- G. Brès
- V. Jaunet
- Sanjiva K. Lele
In Computational Mechanics
- Oliver T. Schmidt
- Aaron Towne
- Tim Colonius
- P. Jordan
- André V. G. Cavalieri
- G. Brès
- V. Jaunet
- Sanjiva K. Lele
In Environmental Engineering
- Tim Colonius
- Oliver T. Schmidt
- Aaron Towne
- P. Jordan
- André V. G. Cavalieri
- G. Brès
- V. Jaunet
- Sanjiva K. Lele
Citations in the corpus
- Acoustic resonance in the potential core of subsonic jets (2017, methodology): “(2017), vol. 825, pp. 1113–1152. c© Cambridge University Press 2017 doi:10.1017/jfm.2017.346 1113 Acoustic resonance in the potential core of subsonic jets Aaron Towne1,†,‡, André V. G. Cavalieri2, Peter Jordan3, Tim Colonius1, Oliver Schmidt1, Vincent Jaunet3 and Guillaume A. Brès4 1Division of Eng”
- Importance of the nozzle-exit boundary-layer state in subsonic turbulent jets (2018, methodology): “The computational set-up is briefly summarized below, with additional details about the solvers, the numerical schemes and the basic methodology available in Brès et al. (2017).”
- Wavepackets and trapped acoustic modes in a turbulent jet: coherent structure eduction and global stability (2017, methodology): “The reader is referred to (Brès et al. 2014, 2015, 2016) for further details and the extensive experimental validation, and to Bodony & Lele (2008) for an overview of the use of LES in jet noise prediction.”
- Spectral analysis of jet turbulence (2017, methodology): “The unstructured flow solver “Charles” (Brès et al. 2017b) is used to perform largeeddy simulations of three turbulent jets at Mach numbers Mj = Uj/aj of 0.4, 0.9, and 1.5.”
- Spectral proper orthogonal decomposition and its relationship to dynamic mode decomposition and resolvent analysis (2017, methodology): “The simulation was performed using the compressible flow solver “Charles” developed at Cascade Technologies (Brès et al., 2017), which solves the spatiallyfiltered compressible Navier-Stokes equations on unstructured grids using a finite-volume method and third-order Runge-Kutta time integration.”