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Investigation of the feedback mechanism in ideally expanded round impinging jets using large-eddy simulation

Gojon, Romain (author)
KTH,Linné Flow Center, FLOW,Laboratoire de Mécanique des Fluides et d’Acoustique, UMR CNRS 5506, Ecole Centrale de Lyon, Ecully, 69134, France
Bogey, C. (author)
Laboratoire de Mécanique des Fluides et d’Acoustique, UMR CNRS 5506, Ecole Centrale de Lyon, Ecully, 69134, France
 (creator_code:org_t)
2016-05-27
2016
English.
In: 22nd AIAA/CEAS Aeroacoustics Conference, 2016. - Reston, Virginia : American Institute of Aeronautics and Astronautics.
  • Conference paper (peer-reviewed)
Abstract Subject headings
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  • Large-eddy simulations (LES) have been performed in order to study the tone generation mechanism in four supersonic ideally expanded round impinging jets. The jets have a Mach number of 1.5, and a Reynolds number of 6 × 104. They impinge normally on a flat plate located at a distance from the nozzle exit varying from 6r0 up to 12r0 where r0 is the jet nozzle radius. The aerodynamic properties of the jets are first investigated. In particular, the convection velocity of the turbulent structures in the jet shear layers is computed. In the spectra of pressure fluctuations in the vicinity of the nozzle exit, intense tones emerge. Their associated Strouhal numbers are in agreement with measurements available for round impinging jets with similar exit conditions. The tone frequencies also correspond well to the frequencies predicted by the classical model of the aeroacoustic feedback establishing between the nozzle lips and the flat plate. A study of the feedback mechanism is then proposed by applying Fourier decomposition to the near pressure fields. The feedback mechanism is found to lead to the formation of hydrodynamic-acoustic standing waves. Moreover, for each tone frequency, the corresponding axisymmetric or helical oscillation mode of the jet is examined. Finally, an analysis is conducted using a vortex sheet model of the jet in order to determine the allowable frequency ranges of the upstream-propagating neutral acoustic wave modes. The tone frequencies obtained in the LES fall within these ranges, depending on their axisymmetric or helical nature.

Subject headings

TEKNIK OCH TEKNOLOGIER  -- Maskinteknik (hsv//swe)
ENGINEERING AND TECHNOLOGY  -- Mechanical Engineering (hsv//eng)

Keyword

Acoustic wave propagation
Aeroacoustics
Aerodynamics
Feedback control
Nozzles
Plates (structural components)
Reynolds number
Shear flow
Supersonic aerodynamics
Acoustic standing wave
Aerodynamic properties
Convection velocity
Fourier decomposition
Near pressure field
Pressure fluctuation
Round impinging jets
Turbulent structures
Large eddy simulation

Publication and Content Type

ref (subject category)
kon (subject category)

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Gojon, Romain
Bogey, C.
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Royal Institute of Technology

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