Published June 2011
| Published
Conference Paper
Open
Hermite Methods for Aeroacoustics: Recent Progress
Abstract
We present recent developments on Hermite methods for aeroacoustic simulations including time-stepping methods, hybridization with discontinuous Galerkin methods for handling of boundary conditions and adaptive implementations. By scaling studies reported below we show that the features unique to Hermite methods have promise to enable efficient exploitation of modern petascale architectures. We also present preliminary computations of turbulent jet noise obtained with the current implementation of our compressible Navier-Stokes solver.
Additional Information
© 2011 by the author(s). Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Published Online: 4 Nov 2012. This material is based upon work supported, in part, by the National Science Foundation under Grants OCI-0905045 and OCI-0904773 and, in part, by ARO grant W911NF-09-1-0344. Any opinions, findings, and conclusions or recommendations expressed in this material are those of the author(s) and do not necessarily reflect the views of the National Science Foundation.Attached Files
Published - AppeloeInkmanHagstromEtAl2011.pdf
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AppeloeInkmanHagstromEtAl2011.pdf
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Additional details
- Eprint ID
- 97188
- Resolver ID
- CaltechAUTHORS:20190717-102317504
- NSF
- OCI-0905045
- NSF
- OCI-0904773
- Army Research Office (ARO)
- W911NF-09-1-0344
- Created
-
2019-07-17Created from EPrint's datestamp field
- Updated
-
2021-11-16Created from EPrint's last_modified field
- Other Numbering System Name
- AIAA Paper
- Other Numbering System Identifier
- 2011-2757