Abstract
A flexible hybrid approach is investigated for computing far-field jet noise. Compressible large eddy simulation based on a linear discontinuous Galerkin (DG) solver is used to com- pute the near-field flow. The far-field noise is computed using a Ffowcs Williams-Hawkings solver. Two variants for the degrees of freedom in the linear DG solver are considered and their impact on the implicit numerical dissipation tested. Both variants support arbitrary, approximately convex polyhedral elements. The overall method is applied to predict the far-field noise of a Ma = 0.9 cold turbulent jet including nozzle geometry. Comparisons with measured flow fields are reasonable, however preliminary noise predictions show excessive falloff in the high frequency range.
| Original language | English |
|---|---|
| Title of host publication | 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition |
| Subtitle of host publication | 5-8 January 2009, Orlando, Florida ; [papers] |
| Publisher | American Institute of Aeronautics and Astronautics |
| ISBN (Print) | 9781563479694 |
| DOIs | |
| Publication status | Published - 1 Dec 2009 |
| Event | 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2009 - Orlando, United States Duration: 5 Jan 2009 → 8 Jan 2009 Conference number: 47 |
Conference
| Conference | 47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2009 |
|---|---|
| Country/Territory | United States |
| City | Orlando |
| Period | 5/01/09 → 8/01/09 |
Fingerprint
Dive into the research topics of 'Noise prediction from cold high-speed turbulent jets using large-eddy simulation'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver