Unsteadiness characterisation of shock wave/turbulent boundary-layer interaction at moderate Reynolds number. (10th January 2023)
- Record Type:
- Journal Article
- Title:
- Unsteadiness characterisation of shock wave/turbulent boundary-layer interaction at moderate Reynolds number. (10th January 2023)
- Main Title:
- Unsteadiness characterisation of shock wave/turbulent boundary-layer interaction at moderate Reynolds number
- Authors:
- Bernardini, Matteo
Della Posta, Giacomo
Salvadore, Francesco
Martelli, Emanuele - Abstract:
- Abstract: Abstract : A direct numerical simulation of an oblique shock wave impinging on a turbulent boundary layer at Mach number 2.28 is carried out at moderate Reynolds number, simulating flow conditions similar to those of the experiment by Dupont et al. ( J. Fluid Mech., vol. 559, 2006, pp. 255–277). The low-frequency shock unsteadiness, whose characteristics have been the focus of considerable research efforts, is here investigated via the Morlet wavelet transform. Owing to its compact support in both physical and Fourier spaces, the wavelet transformation makes it possible to track the time evolution of the various scales of the wall-pressure fluctuations. This property also makes it possible to define a local intermittency measure, representing a frequency-dependent flatness factor, to pinpoint the bursts of energy that characterise the shock intermittency scale by scale. As a major result, wavelet decomposition shows that the broadband shock movement is actually the result of a collection of sparse events in time, each characterised by its own temporal scale. This feature is hidden by the classical Fourier analysis, which can only show the time-averaged behaviour. Then, we propose a procedure to process any relevant time series, such as the time history of the wall pressure or that of the separation bubble extent, in which we use a condition based on the local intermittency measure to filter out the turbulent content in the proximity of the shock foot and to isolateAbstract: Abstract : A direct numerical simulation of an oblique shock wave impinging on a turbulent boundary layer at Mach number 2.28 is carried out at moderate Reynolds number, simulating flow conditions similar to those of the experiment by Dupont et al. ( J. Fluid Mech., vol. 559, 2006, pp. 255–277). The low-frequency shock unsteadiness, whose characteristics have been the focus of considerable research efforts, is here investigated via the Morlet wavelet transform. Owing to its compact support in both physical and Fourier spaces, the wavelet transformation makes it possible to track the time evolution of the various scales of the wall-pressure fluctuations. This property also makes it possible to define a local intermittency measure, representing a frequency-dependent flatness factor, to pinpoint the bursts of energy that characterise the shock intermittency scale by scale. As a major result, wavelet decomposition shows that the broadband shock movement is actually the result of a collection of sparse events in time, each characterised by its own temporal scale. This feature is hidden by the classical Fourier analysis, which can only show the time-averaged behaviour. Then, we propose a procedure to process any relevant time series, such as the time history of the wall pressure or that of the separation bubble extent, in which we use a condition based on the local intermittency measure to filter out the turbulent content in the proximity of the shock foot and to isolate only the intermittent component of the signal. In addition, wavelet analysis reveals the intermittent behaviour also of the breathing motion of the recirculation bubble behind the reflected shock, and allows us to detect a direct, partial correspondence between the most significant intermittent events of the separation region and those of the wall pressure at the foot of the shock. … (more)
- Is Part Of:
- Journal of fluid mechanics. Volume 954(2023)
- Journal:
- Journal of fluid mechanics
- Issue:
- Volume 954(2023)
- Issue Display:
- Volume 954, Issue 2023 (2023)
- Year:
- 2023
- Volume:
- 954
- Issue:
- 2023
- Issue Sort Value:
- 2023-0954-2023-0000
- Page Start:
- Page End:
- Publication Date:
- 2023-01-10
- Subjects:
- compressible boundary layers -- shock waves -- supersonic flow
Fluid mechanics -- Periodicals
532.005 - Journal URLs:
- http://www.journals.cambridge.org/jid%5FFLM ↗
http://firstsearch.oclc.org ↗ - DOI:
- 10.1017/jfm.2022.1038 ↗
- Languages:
- English
- ISSNs:
- 0022-1120
- Deposit Type:
- Legaldeposit
- View Content:
- Available online (eLD content is only available in our Reading Rooms) ↗
- Physical Locations:
- British Library HMNTS - ELD Digital store
- Ingest File:
- 26961.xml