Analysis of the Dominant Structures of an Impinging Round Jet at M=0.9

Large-eddy simulation of subsonic round jet impinging on a flat circular plate is performed at Mach number 0.9 and Reynolds number 25,000, based on the diameter and centerline velocity of the jet for two impingement distances [Formula: see text] of [Formula: see text] and [Formula: see text] using h...

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Bibliographic Details
Published in:AIAA journal 2024-02, Vol.62 (2), p.1-18
Main Authors: Pradhan, Swagatika, Thaker, Parth, Ghosh, Somnath
Format: Article
Language:English
Subjects:
Circular plates
Finite difference method
Fluid flow
Jet impingement
Large eddy simulation
Mach number
Power spectral density
Reynolds number
Stagnation point
Wall jets
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Summary:Large-eddy simulation of subsonic round jet impinging on a flat circular plate is performed at Mach number 0.9 and Reynolds number 25,000, based on the diameter and centerline velocity of the jet for two impingement distances [Formula: see text] of [Formula: see text] and [Formula: see text] using high-order compact finite difference scheme. The complex flow phenomena associated with the impinging jet flowfield are studied. The power spectral density (PSD) of instantaneous pressure reveals a discrete impingement tone. Dynamic mode decomposition (DMD) of the velocity and pressure is also done for both cases to extract the most dominant modes of the flow. The fundamental impingement tone frequency obtained from the PSD of pressure is identical to that of the first dominant pressure mode obtained from DMD. Both axisymmetric and semihelical modes are present for the [Formula: see text] case, but only axisymmetric modes are there in the [Formula: see text] case, and it is noted that the modes corresponding to the fundamental tone have an axisymmetric structure. Also, one dominant mode showing the wall jet structures denoting the liftoff of fluid from the wall after impingement at some radial distance away from the stagnation region is present in both impingement distance cases.
ISSN:0001-1452
1533-385X
DOI:10.2514/1.J063282