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University of Illinois at Urbana-Champaign

Resolvent-based framework for jet noise reduction of a low bypass ratio coannular nozzle

Abstract

dc:description

The development of jet noise reduction (JNR) techniques is critical to the integration of supersonic aircraft into commercial travel and transportation. Prescribing JNR methods remains inherently difficult as the reduction of sound is frequently accompanied by a reduction in nozzle performance. This paper utilizes resolvent analysis as a reduced-order modeling technique for the purpose of assessing jet noise reduction concepts on a low bypass ratio coannular nozzle design. An automated framework is built to facilitate the computation of resolvent gain values for varying nozzle conditions and geometries. Specifically, parametric studies are conducted on the mixing duct length and extraction ratio parameters of the nozzle design. RANS mean flow data, used as input for the resolvent computation, are validated against experimental data for the same nozzle configuration. Verification of the linear operator used to define the resolvent is established through comparisons with well-known analytical solutions. Subsequently, the resolvent analysis is verified by comparing sets of singular values and forcing/response modes against corresponding plots reported in the literature. Gain profiles computed for a range of nozzle mixing duct lengths are found to be insensitive to this design parameter. Likewise, gain profiles are also found to be insensitive to variations in extraction ratio at constant thrust. Both of these behaviors are found to be consistent with experimental data suggesting an insubstantial change in noise when varying these nozzle operating parameters. Applying resolvent analysis as a means to assess JNR potential shows promise for comparative design studies, though other nozzle designs and/or operating conditions are needed to positively affirm this.

Degree

thesis:*
Name thesis:degree_name
M.S.
Level thesis:degree_level
Thesis
Discipline thesis:degree_discipline
Aerospace Engineering
Grantor
University of Illinois at Urbana-Champaign
Year dc:date
2023

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Woo, Jaywon
Contributors dc:contributor
  • Bodony, Daniel J

Subjects

dc:subject × 6

Rights

dc:rights
Statement dc:rights
  • Copyright 2023 Jaywon Woo
Language dc:language
en, eng

Identifiers

dc:identifier.*
Handle dc:identifier
https://hdl.handle.net/2142/121372

Chain of custody

source
Harvested from
University of Illinois - Urbana-Champaign
Base URL
www.ideals.illinois.edu/oai-pmh
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Woo, Jaywon. Resolvent-based framework for jet noise reduction of a low bypass ratio coannular nozzle. Thesis thesis, University of Illinois at Urbana-Champaign, 2023. https://hdl.handle.net/2142/121372