Numerical simulation of a Mach 1.92 turbulent jet and its sound field
By Jonathan B. Freund, Sanjiva K. Lele, Parviz Moin. 2000
189 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics, Environmental Engineering
View Paper: https://www.semanticscholar.org/paper/328c046bb60438ef0fb5cac8d2e585a239560578
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
- Sanjiva K. Lele
- Christophe Bogey
- Christophe Bailly
- Tim Colonius
- Meng Wang
- Jonathan B. Freund
- P. Jordan
- D. Juvé
In Computational Mechanics
- Sanjiva K. Lele
- Christophe Bailly
- Christophe Bogey
- Tim Colonius
- Meng Wang
- Jonathan B. Freund
- P. Jordan
- D. Juvé
In Environmental Engineering
- Tim Colonius
- Sanjiva K. Lele
- Christophe Bogey
- Christophe Bailly
- Meng Wang
- Jonathan B. Freund
- P. Jordan
- D. Juvé
Citations in the corpus
- COMPUTATIONAL PREDICTION OF FLOW-GENERATED SOUND (2006, methodology): “Numerical means of solution extension typically involve solving simplified equations, such as the linearized Euler equations or wave equation, in a larger domain external to the domain of direct simulation (Freund et al. 2000).”
- Computational aeroacoustics: progress on nonlinear problems of sound generation (2004, methodology): “If a different equation set is used in the extended domain it is necessary to ensure that accurate and stable transfer of information is achieved at the grid interface (e.g. Freund et al. [43]).”
- Noise Investigation of a High Subsonic, Moderate Reynolds Number Jet Using a Compressible Large Eddy Simulation (2003, methodology): “The first applications of DNS to compute noise for three-dimensional flows were performed by Freund et al. (2000) and Freund (2001) on supersonic and subsonic round jets respectively, with ReD = 3600 for the subsonic jet.”