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Large-eddy simulations of flow and aeroacoustics of twin square jets including turbulence tripping

Ahn, MyeongHwan (author)
KTH,Teknisk mekanik,Linné Flow Center, FLOW
Mihaescu, Mihai, Professor, 1976- (author)
KTH,Linné Flow Center, FLOW,Strömningsmekanik och Teknisk Akustik
Karnam, Aatresh (author)
University of Cincinnati
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Gutmark, Ephraim (author)
Aerospace Engineering, University of Cincinnati
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 (creator_code:org_t)
AIP Publishing, 2023
2023
English.
In: Physics of fluids. - : AIP Publishing. - 1070-6631 .- 1089-7666. ; 35:6
  • Journal article (peer-reviewed)
Abstract Subject headings
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  • In this study, we investigate the flow and aeroacoustics of twin square (i.e., aspect ratio of 1.0) jets by implicit large-eddy simulations (LESs) under a nozzle pressure ratio of 3.0 and a temperature ratio of 1.0 conditions. A second-order central scheme coupled with a modified Jameson's artificial dissipation is used to resolve acoustics as well as to capture discontinuous solutions, e.g., shock waves. The flow boundary layer inside of the nozzle is tripped, using a small step in the convergent section of the nozzle. The time-averaged axial velocity and turbulent kinetic energy of LES with boundary layer tripping approaches better to particle image velocimetry experimental data than the LES without turbulence tripping case. A two-point space–time cross-correlation analysis suggests that the twin jets are screeching and are coupled to each other in a symmetrical flapping mode. Intense pressure fluctuations and standing waves are observed between the jets. Spectral proper orthogonal decomposition (SPOD) confirms the determined mode and the relevant wave propagation. The upstream propagating mode associated with the shock-cell structures is confined inside jets. Far-field noise obtained by solving Ffowcs Williams and Hawkings equation is in good agreement with the measured acoustic data. The symmetrical flapping mode of twin jets yields different levels of the screech tone depending on observation planes. The tonalities—the fundamental tone, second and third harmonics—appear clearly in the far-field, showing different contributions at angles corresponding to the directivities revealed by SPOD.

Subject headings

TEKNIK OCH TEKNOLOGIER  -- Maskinteknik -- Strömningsmekanik och akustik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering -- Fluid Mechanics and Acoustics (hsv//eng)
TEKNIK OCH TEKNOLOGIER  -- Maskinteknik -- Rymd- och flygteknik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering -- Aerospace Engineering (hsv//eng)

Keyword

Large-eddy simulations; supersonic jets; aeroacoustics; twin square jets; turbulence tripping
Teknisk mekanik
Engineering Mechanics
Aerospace Engineering
Flyg- och rymdteknik

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Ahn, MyeongHwan
Mihaescu, Mihai, ...
Karnam, Aatresh
Gutmark, Ephraim
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