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Role of non-linearities induced by deterministic forcing in the low-frequency dynamics of transitional shock wave/boundary layer interaction

Role of non-linearities induced by deterministic forcing in the low-frequency dynamics of transitional shock wave/boundary layer interaction
Role of non-linearities induced by deterministic forcing in the low-frequency dynamics of transitional shock wave/boundary layer interaction
Direct numerical simulations are carried out to investigate the underlying mechanism of the low-frequency unsteadiness of a transitional shock reflection with separation at M=1.5. To clarify the nonlinear mechanisms, the incoming laminar boundary layer is forced with two different arrangements of oblique unstable modes. Each wave arrangement is given by a combination of two unstable waves such that their difference in frequency falls in a low-frequency range corresponding to a Strouhal number (based on the length of interaction) of 0.04. This deterministic forcing allows the introduction of nonlinearities, and high-order statistical tools are used to identify the properties of quadratic couplings. It is found that the low-frequency unsteadiness and the transition to turbulence are decoupled problems. On the one hand, the unstable modes of the boundary layer interact nonlinearly such that energy cascades to higher frequencies, initiating the turbulent cascade process, and to lower frequencies. On the other hand, the low-frequency quadratic coupling of the oblique modes is found to be responsible for low-frequency unsteadiness affecting the separation point. The direction of the quadratic interactions is extracted and it is shown that, in the presence of low-frequency unsteadiness, these interactions enter the separated zone just before reattachment and travel both downstream and upstream, extending beyond the separation point, hence feeding the low-frequency bubble response. In addition to the two main arrangements of oblique modes, two other combinations are analysed, including multiple oblique waves and streaks. Interestingly, their inclusion did not alter the low-frequency unsteadiness phenomenon. Furthermore, the effect of the forcing difference frequency is examined and it is shown that the breathing phenomenon is sensitive to the range of frequencies present in the system due to a low-pass filter effect.
boundary layer separation, compressible boundary layers, turbulent transition
0022-1120
Mauriello, Mariadebora
df284ddb-4cf7-41d6-b136-05cf2a714a00
Sharma, Pushpender K.
31c7280b-e564-46cb-ad1a-bb7fa00f3887
Larcheveque, Lionel
fcb9a731-4546-4139-bd3d-a21084f0450a
Sandham, Neil
0024d8cd-c788-4811-a470-57934fbdcf97
Mauriello, Mariadebora
df284ddb-4cf7-41d6-b136-05cf2a714a00
Sharma, Pushpender K.
31c7280b-e564-46cb-ad1a-bb7fa00f3887
Larcheveque, Lionel
fcb9a731-4546-4139-bd3d-a21084f0450a
Sandham, Neil
0024d8cd-c788-4811-a470-57934fbdcf97

Mauriello, Mariadebora, Sharma, Pushpender K., Larcheveque, Lionel and Sandham, Neil (2025) Role of non-linearities induced by deterministic forcing in the low-frequency dynamics of transitional shock wave/boundary layer interaction. Journal of Fluid Mechanics, 1016, [A6]. (doi:10.1017/jfm.2025.10385).

Record type: Article

Abstract

Direct numerical simulations are carried out to investigate the underlying mechanism of the low-frequency unsteadiness of a transitional shock reflection with separation at M=1.5. To clarify the nonlinear mechanisms, the incoming laminar boundary layer is forced with two different arrangements of oblique unstable modes. Each wave arrangement is given by a combination of two unstable waves such that their difference in frequency falls in a low-frequency range corresponding to a Strouhal number (based on the length of interaction) of 0.04. This deterministic forcing allows the introduction of nonlinearities, and high-order statistical tools are used to identify the properties of quadratic couplings. It is found that the low-frequency unsteadiness and the transition to turbulence are decoupled problems. On the one hand, the unstable modes of the boundary layer interact nonlinearly such that energy cascades to higher frequencies, initiating the turbulent cascade process, and to lower frequencies. On the other hand, the low-frequency quadratic coupling of the oblique modes is found to be responsible for low-frequency unsteadiness affecting the separation point. The direction of the quadratic interactions is extracted and it is shown that, in the presence of low-frequency unsteadiness, these interactions enter the separated zone just before reattachment and travel both downstream and upstream, extending beyond the separation point, hence feeding the low-frequency bubble response. In addition to the two main arrangements of oblique modes, two other combinations are analysed, including multiple oblique waves and streaks. Interestingly, their inclusion did not alter the low-frequency unsteadiness phenomenon. Furthermore, the effect of the forcing difference frequency is examined and it is shown that the breathing phenomenon is sensitive to the range of frequencies present in the system due to a low-pass filter effect.

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Accepted/In Press date: 16 June 2025
e-pub ahead of print date: 28 July 2025
Keywords: boundary layer separation, compressible boundary layers, turbulent transition

Identifiers

Local EPrints ID: 503512
URI: http://eprints.soton.ac.uk/id/eprint/503512
ISSN: 0022-1120
PURE UUID: 0938d240-6d4c-47a4-ba10-78c0c3128166
ORCID for Pushpender K. Sharma: ORCID iD orcid.org/0000-0003-2078-2559
ORCID for Neil Sandham: ORCID iD orcid.org/0000-0002-5107-0944

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Date deposited: 04 Aug 2025 16:48
Last modified: 01 Oct 2025 02:05

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Contributors

Author: Mariadebora Mauriello
Author: Lionel Larcheveque
Author: Neil Sandham ORCID iD

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