Abstract

Wall-model large eddy simulations (WMLES) are conducted to investigate the spatial features of large-scale and very-large-scale motions (LSMs and VLSMs) in turbulent boundary flow in different surface roughnesses at a very high Reynolds number, O (106–107). The results of the simulation of nearly smooth cases display good agreement with field observations and experimental data, both dimensioned using inner and outer variables. Using pre-multiplied spectral analysis, the size of VLSMs can be reduced or even disappear with increasing roughness, which indirectly supports the concept that the bottom-up mechanism is one of the origins of VLSMs. With increases in height, the power of pre-multiplied spectra at both high and low wavenumber regions decreases, which is consistent with most observational and experimental results. Furthermore, we find that the change in the spectrum scaling law from −1 to −5/3 is a gradual process. Due to the limitations of the computational domain and coarse grid that were adopted, some VLSMs and small-scale turbulence are truncated. However, the size of LSMs is fully accounted for. From the perspective of the spatial correlation of the flow field, the structural characteristics of VLSMs under various surface roughnesses, including three-dimensional length scales and inclination angles, are obtained intuitively, and the conclusions are found to be in good agreement with the velocity spectra. Finally, the generation, development and extinction of three-dimensional VLSMs are analyzed by instantaneous flow and vorticity field, and it shows that the instantaneous flow field gives evidence of low-speed streamwise-elongated flow structures with negative streamwise velocity fluctuation component, and which are flanked on each side by similarly high-speed streamwise-elongated flow structures. Moreover, each of the low-speed streamwise-elongated flow structure lies beneath many vortices.

Highlights

  • Large-scale and very-large-scale motions (LSMs and VLSMs) exist in pipe flow, channel flow, and turbulent boundary layer (TBL) flow

  • Lee et al [6] investigated the spatial features of LSMs and VLSMs in a turbulent channel flow with a direct numerical simulation (DNS) of Reτ = 930, the results indicating that the streamwise length of the VLSMs linearly determines the number of outer LSMs and that the formation of VLSMs possibly comes from the alignment of the positive and negative streamwise-fluctuation structures

  • LSMs and VLSMsregion, structures the inclination angles at A and B do not exist at line C, this indicates that LSMs and VLSMs structures located at low momentum region, and comes from the near wall aligned packets, as described by “bottom-up” mechanism

Read more

Summary

Introduction

Large-scale and very-large-scale motions (LSMs and VLSMs) exist in pipe flow, channel flow, and turbulent boundary layer (TBL) flow. Lee and Sung [8] conducted DNS simulations of a TBL flow, with a momentum height Reynolds number of up to Reθ = 2560 They showed that the development process of adjacent packet-type structures combines to form VLSMs, and they employed a modified feature-extraction algorithm to identify the properties of the VLSMs. Lee et al [6] investigated the spatial features of LSMs and VLSMs in a turbulent channel flow with a DNS of Reτ = 930, the results indicating that the streamwise length of the VLSMs linearly determines the number of outer LSMs and that the formation of VLSMs possibly comes from the alignment of the positive and negative streamwise-fluctuation structures.

Numerical Method
Simulation Setup
Validation by Non-Dimensional
Morgan
Validation by Non-Dimensional Outer Variables
Comparison of outer-scaled height simulation with the experimental in results
Streamwise
The height indicators for each graph are the as those shown in Figure
12. The trend for wall-normal fluctuation spectraspectra are shown
Flow Field Correlation Analysis
Instantaneous Flow Field Analysis
16. Inheight
The Generation and Development of VLSMs
For dashed
19. Evidence
Vortices Field Analysis
22. Instantaneous
Conclusions

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.