CaltechAUTHORS
Published 2010 | Version Published
Journal Article Open

Development of Arbitrary-Order Hermite Methods for Simulation and Analysis of Turbulent Jet Noise

Creators

Abstract

In this short note a brief description of Hermite methods is given. Previous and ongoing development of arbitrary order Hermite methods for the simulation of turbulent jets is also presented. In addition we outline how Hermite methods can be hybridized with discontinuous Galerkin methods to handle boundary conditions in a straightforward way.

Additional Information

© 2010 Published by Elsevier Ltd. Under a Creative Commons license (Attribution-NonCommercial-NoDerivs 3.0 Unported (CC BY-NC-ND 3.0)). Available online 7 October 2010. The authors were funded by NSF grant 0905045.

Attached Files

Published - Appeloe2010p13184Iutam_Symposium_On_Computational_Aero-Acoustics_For_Aircraft_Noise_Prediction.pdf

Files

Appeloe2010p13184Iutam_Symposium_On_Computational_Aero-Acoustics_For_Aircraft_Noise_Prediction.pdf

Files (866.8 kB)

Additional details

Identifiers

Eprint ID
23003
Resolver ID
CaltechAUTHORS:20110321-092415409

Funding

NSF
OAC-0905045

Dates

Created
2011-03-21
Created from EPrint's datestamp field
Updated
2021-11-09
Created from EPrint's last_modified field

Caltech Custom Metadata

Series Name
Procedia Engineering