Aeroacoustics of hot jets
By K. Viswanathan. Journal of Fluid Mechanics, 2002
329 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Atmospheric Science, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/7462492e21e77b1ce5d4d38423d0bb29d2d81748
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
- Tim Colonius
- P. Jordan
- Oliver T. Schmidt
- Aaron Towne
- G. Brès
- André V. G. Cavalieri
- Sanjiva K. Lele
- Christopher K. W. Tam
In Atmospheric Science
- P. Jordan
- Sanjiva K. Lele
- Tim Colonius
- Daniel J. Bodony
- Christopher K. W. Tam
- J. Panda
- K. Ahuja
- Oliver T. Schmidt
In Computational Mechanics
- Tim Colonius
- P. Jordan
- Oliver T. Schmidt
- Aaron Towne
- G. Brès
- André V. G. Cavalieri
- Sanjiva K. Lele
- Christopher K. W. Tam
Citations in the corpus
- Mach Wave Radiation from High-Speed Jets (2009, background): “[9] andViswanathan [10].”
- Acoustic resonance in the potential core of subsonic jets (2017, background): “Turbulent jets at high subsonic Mach number are relevant to commercial aircraft noise and have been the subject of recent experiments (Viswanathan 2004; Hileman et al. 2005; Suzuki & Colonius 2006; Cavalieri et al. 2013; Fontaine et al. 2015) and large-eddy simulations (Bodony & Lele 2008; Bogey &…”
- Wave Packets and Turbulent Jet Noise (2013, methodology): “The recent experiments of Viswanathan et al. (2011) utilized 294 microphones placed along a half-cone of angle 10◦ to study near-field pressure fluctuations.”
- Current Status of Jet Noise Predictions Using Large-Eddy Simulation (2008, methodology): “[16], overpredict the higher Reynolds number data of Tanna [81] and Viswanathan [83] at low angles and underpredict at larger observer angles.”
- The sources of jet noise: experimental evidence (2007, methodology): “However, based on his extensive jet noise data analysis, Viswanathan (2004, 2006) showed that his data fitted a generalized power law of the form,”
- Unstructured Large-Eddy Simulations of Supersonic Jets (2017, background): “Experiments [51] and simulations [1,33] indicated that jet noise was insensitive to Reynolds number above a critical Reynolds number of approximately 10(5).”