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Large eddy simulation for jet noise: the importance of getting the boundary layer right

Brès, Guillaume A. and Jaunet, Vincent and Le Rallic, Maxime and Jordan, Peter and Colonius, Tim and Lele, Sanjiva K. (2015) Large eddy simulation for jet noise: the importance of getting the boundary layer right. In: 21st AIAA/CEAS Aeroacoustics Conference, 22-26 June 2015, Dallas, TX. https://resolver.caltech.edu/CaltechAUTHORS:20190712-112322014

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Abstract

Large eddy simulations of an isothermal Mach 0.9 jet issued from a convergent-straight nozzle are performed at Reynolds number 1 × 10^6. The flow configuration and operating conditions match the companion experiment conducted at the PPRIME Institute, Poitiers. To replicate the effects of the boundary layer trip present in the experiment and to ensure a turbulent jet, localized adaptive mesh refinement, synthetic turbulence, and wall modeling are used inside the nozzle. This leads to fully turbulent nozzle-exit boundary layers and results in significant improvements for the flow field and sound predictions, compared to those obtained from the typical approach based on laminar flow assumption in the nozzle. The far-field noise spectra now match the experimental measurements to within 0.5 dB for relevant angles and frequencies. As a next step toward better understanding of turbulent jet noise, the large database collected during the simulation is currently being used for reduced order modeling and wavepacket analysis.


Item Type:Conference or Workshop Item (Paper)
Related URLs:
URLURL TypeDescription
https://doi.org/10.2514/6.2015-2535DOIConference Paper
https://arc.aiaa.org/doi/10.2514/6.2015-2535PublisherConference Paper
ORCID:
AuthorORCID
Brès, Guillaume A.0000-0003-2507-8659
Jordan, Peter0000-0001-8576-5587
Colonius, Tim0000-0003-0326-3909
Additional Information:© 2015 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Published Online: 18 Jun 2015. The preliminary LES studies were supported by NAVAIR SBIR project, under the supervision of Dr. John T. Spyropoulos. The main calculations were carried out on CRAY XE6 machines at DoD supercomputer facilities in ERDC DSRC. P. Jordan acknowledges the support of the French National Research Agency (ANR) through the project COOLJAZZ. Part of this work was performed during the Center for Turbulence Research Summer Program 2014 at Stanford University.
Funders:
Funding AgencyGrant Number
Naval Air Systems Command (NAVAIR)UNSPECIFIED
Agence Nationale pour la Recherche (ANR)COOLJAZZ
Subject Keywords:Aeroacoustics
Other Numbering System:
Other Numbering System NameOther Numbering System ID
AIAA Paper2015-2535
Record Number:CaltechAUTHORS:20190712-112322014
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20190712-112322014
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:97111
Collection:CaltechAUTHORS
Deposited By: Melissa Ray
Deposited On:15 Jul 2019 18:33
Last Modified:03 Oct 2019 21:28

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