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Effects of Screech on Jet Coupling in Twin Square Jets
University of Cincinnati.
KTH, School of Engineering Sciences (SCI), Engineering Mechanics.ORCID iD: 0000-0002-9054-8832
Aerospace Engineering, University of Cincinnati.
KTH, School of Engineering Sciences (SCI), Engineering Mechanics, Fluid Mechanics and Engineering Acoustics.ORCID iD: 0000-0001-7330-6965
2022 (English)In: 28th AIAA/CEAS Aeroacoustics Conference, 2022 / [ed] AIAA, American Institute of Aeronautics and Astronautics (AIAA) , 2022, article id AIAA 2022-3067Conference paper, Published paper (Refereed)
Abstract [en]

The coupling of square convergent divergent jets in Twin Jet configuration undergoing screech is investigated. Particle Image Velocimetry, high speed Schlieren imaging techniques & Large Eddy Simulations were employed to study qualitative & quantitative aspects of the coupled jet interactions. Comparisons between experimental & computational data were drawn to elucidate the observations made in experimental results & probe the driving cause of the coupling phenomenon. Twin square jets were found to exhibit symmetric flapping motion mirrored about the nozzle symmetry plane. Strong acoustic propagation driven by phase locked shear layer interactions between the jet were observed driving flow propagation in upstream & downstream directions. Tone propagation into the ambient was driven by out of phase flapping of the outer shear layers of the jet. Near field acoustic measurements showed multiple harmonic tones driven by screech & subharmonic tones generated due to coupled shear layer interactions. Flow field results revealed branched turbulence distribution along the inner shear layers as a result of the strong flapping.

Place, publisher, year, edition, pages
American Institute of Aeronautics and Astronautics (AIAA) , 2022. article id AIAA 2022-3067
Keywords [en]
Supersonic Twin Jets, screech, flow instabilities, Particle Image Velocimetry, Schlieren imaging, Large Eddy Simulations
National Category
Vehicle and Aerospace Engineering Fluid Mechanics
Research subject
Aerospace Engineering; Engineering Mechanics
Identifiers
URN: urn:nbn:se:kth:diva-315296DOI: 10.2514/6.2022-3067Scopus ID: 2-s2.0-85135062101OAI: oai:DiVA.org:kth-315296DiVA, id: diva2:1679528
Conference
28th AIAA/CEAS Aeroacoustics Conference, 2022, 28th AIAA/CEAS Aeroacoustics Conference, 2022, Southampton, 14 June 2022 through 17 June 2022
Note

QC 20220819

Part of proceedings: ISBN 978-162410664-4

Available from: 2022-07-01 Created: 2022-07-01 Last updated: 2026-03-12Bibliographically approved

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Ahn, MyeongHwanMihaescu, Mihai

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