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Evaluation of PSE as a Model for Supersonic Jet Using Transfer Functions

Kleine, Vitor G. and Sasaki, Kenzo and Cavalieri, André V. G. and Brès, Guillaume A. and Colonius, Tim (2017) Evaluation of PSE as a Model for Supersonic Jet Using Transfer Functions. In: 23rd AIAA/CEAS Aeroacoustics Conference, 5-9 June 2017, Denver, CO. https://resolver.caltech.edu/CaltechAUTHORS:20190709-092059023

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Abstract

Parabolized Stability Equations (PSE) have been shown to model wavepackets and, consequently, the near field of turbulent jets with reasonable accuracy. Because of these capabilities, PSE is a promising reduced-order model to derive control laws that could be employed to reduce the sound generation of a jet. The purpose of this work is to apply PSE to obtain time-domain transfer functions that could estimate both the fluid-dynamic and the acoustic fields of a supersonic jet. The results of this model were compared to results obtained from a database of a well-validated large-eddy simulation of a supersonic jet. Based on the unsteady pressure data at a input position, the time-domain pressure field was estimated using transfer functions obtained using PSE and an empirical method based on the LES data. The prediction scheme employed is a single-input-single-output (SISO), linear model. The unsteady pressure predicted by PSE showed good agreement with the LES results, especially if the input position is outside the mixing layer. For this region, the prediction capabilities of PSE are comparable to those of empirical transfer functions. The agreement is good even for output points taken in the acoustic field, showing that it is possible to estimate the time-domain behaviour of Mach-wave radiation using transfer functions. This indicates that PSE could not only be used to predict the sound generation, but also to open up new potentialities to attenuate noise by means of closed-loop control of the flow. The exploration of the regions where the method displayed good agreement, presented in this work, can guide the positioning of sensors and actuators for experimental implementation of closed-loop control in a jet.


Item Type:Conference or Workshop Item (Paper)
Related URLs:
URLURL TypeDescription
https://doi.org/10.2514/6.2017-4194DOIConference Paper
https://arc.aiaa.org/doi/10.2514/6.2017-4194PublisherConference Paper
ORCID:
AuthorORCID
Sasaki, Kenzo0000-0002-3347-4996
Brès, Guillaume A.0000-0003-2507-8659
Colonius, Tim0000-0003-0326-3909
Additional Information: © 2017 by André Valdetaro Gomes Cavalieri. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. Published Online: 2 Jun 2017. This work has been funded by CNPq (grant number 444796/2014-2). A. Cavalieri was supported by a CNPq research scholarship. Kenzo Sasaki acknowledges the financial support from Capes via a PhD scholarship.
Funders:
Funding AgencyGrant Number
Conselho Nacional de Desenvolvimento Científico e Tecnológico (CNPq)444796/2014-2
Coordenação de Aperfeiçoamento de Pessoal de Nível Superior (CAPES)UNSPECIFIED
Other Numbering System:
Other Numbering System NameOther Numbering System ID
AIAA Paper2017-4194
Record Number:CaltechAUTHORS:20190709-092059023
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20190709-092059023
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:96951
Collection:CaltechAUTHORS
Deposited By: Melissa Ray
Deposited On:09 Jul 2019 22:46
Last Modified:03 Oct 2019 21:26

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