Noise Prediction for Increasingly Complex Jets. Part I: Methods and Tests

By M. Shur, P. Spalart, M. Strelets. 2005

386 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/1300f70144c14cea462a2d3b19e68e2251ac7952

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. Oliver T. Schmidt
2. Aaron Towne
3. Tim Colonius
4. P. Jordan
5. G. Brès
6. André V. G. Cavalieri
7. V. Jaunet
8. Sanjiva K. Lele

In Computational Mechanics

1. Oliver T. Schmidt
2. Aaron Towne
3. Tim Colonius
4. P. Jordan
5. G. Brès
6. André V. G. Cavalieri
7. V. Jaunet
8. Sanjiva K. Lele

Citations in the corpus

• Importance of the nozzle-exit boundary-layer state in subsonic turbulent jets (2018, methodology): “H outflow disk, the method of ‘end-caps’ of Shur et al. (2005a) is applied for x> 25D, where the complex far-field pressures predicted from 11 FW–”
• Unstructured Large-Eddy Simulations of Supersonic Jets (2017, methodology): “Starting from the study in [13], their work showed a”