Skip to main content
Log in

Wake flow evolution behind a circular cylinder with two perpendicular slits at various angles of attack

  • Regular Paper
  • Published:
Journal of Visualization Aims and scope Submit manuscript

Abstract

A wind tunnel experiment was performed to study the wake vortex dynamic behind a circular cylinder with two perpendicular slits (TPS) using time-resolved particle image velocimetry. The experimental studies were conducted at a Reynolds number of 1767 based on the incoming airflow and the diameter of the circular cylinder. The slit was built in the circular cylinder with a width of 0.08D (D is the diameter of the circular cylinder). The angles of attack were set from 0° to 45° from the incoming airflow direction. The time-average result, such as turbulence kinetic energy, streamline, and normalized Reynolds shear stress, were investigated to illustrate the influence of the angles of attack on the wake flow. The evolution of wake vortex shedding at one period was divided into four phases based on proper orthogonal decomposition analysis. This suggests that the wake vortex shedding behind the circular cylinder with TPS at various angles of attack exhibits notable modifications compared to the uncontrolled case. The mean velocity at the point of the wake slit hole revealed a jet flow blowing out from the slit and interacting with the wake flow. Moreover, the effect of drag coefficient reduction was estimated owing to TPS.

Graphical abstract

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11
Fig. 12
Fig. 13

Similar content being viewed by others

References

  • Banerjee A, Gurugubelli PS, Kumar N, Jaiman RK (2021) Influence of flexible fins on vortex-induced load over a circular cylinder at low Reynolds number. Phys Fluids 33(11):113602

    Article  Google Scholar 

  • Bohl DG, Koochesfahani MM (2009) MTV measurements of the vortical field in the wake of an airfoil oscillating at high reduced frequency. J Fluid Mech 620:63–88

    Article  MATH  Google Scholar 

  • Chen GB, Chen WL (2022) Experimental investigation and validation on suppressing the unsteady aerodynamic force and flow structure of single box girder by trailing edge jets. Appl Sci Basel 12(3):967

    Article  Google Scholar 

  • Chen WL, Xin DB, Xu F, Li H, Ou JP, Hu H (2013) Suppression of vortex-induced vibration of a circular cylinder using suction-based flow control. J Fluid Struct 42(4):25–39

    Article  Google Scholar 

  • Chen WL, Li H, Hu H (2014) An experimental study on a suction flow control method to reduce the unsteadiness of the wind loads acting on a circular cylinder. Exp Fluids 55(4):1–20

    Article  Google Scholar 

  • Chen WL, Gao DL, Yuan WY, Li H, Hu H (2015) Passive jet control of flow around a circular cylinder. Exp Fluids 56(11):201

    Article  Google Scholar 

  • Chen WL, Chen GB, Xu F, Huang YW, Gao DL, Li H (2020) Suppression of vortex-induced vibration of a circular cylinder by a passive-jet flow control. J Wind Eng Ind Aerodyn 199:104119

    Article  Google Scholar 

  • Chen GB, Chen WL, Gao DL, Yang ZF (2021) Active control of flow structure and unsteady aerodynamic force of box girder with leading-edge suction and trailing-edge jet. Exp Therm Fluid Sci 120:110244

    Article  Google Scholar 

  • Chen ZW, Ni YQ, Wang YW, Wang SM, Liu TH (2022a) Mitigating crosswind effect on high-speed trains by active blowing method: a comparative study. Eng Appl Comput Fluid 16(1):1064–1081

    Google Scholar 

  • Chen GB, Chen WL, Min XW, Gao DL (2022b) A coupled model for vortex induced vibration of a circular cylinder with and without passive-jet flow control. J Fluids Struct 110:103541

    Article  Google Scholar 

  • Choi H, Jeon WP, Kim J (2008) Control of flow over a bluff body. Annu Rev Fluid Mech 40:113–139

    Article  MathSciNet  MATH  Google Scholar 

  • Corke TC, Enloe CL, Wilkinson SP (2010) Dielectric barrier discharge plasma actuators for flow control. Annu Rev Fluid Mech 42:505–529

    Article  Google Scholar 

  • Du H, Zhang Q, Li Q, Kong W, Yang L (2022) Drag reduction in cylindrical wake flow using porous material. Phys Fluids 34(4):045102

    Article  Google Scholar 

  • Dusek J, Le Gal P, Fraunie P (1994) A numerical and theoretical study of the first hopf bifurcation in a cylinder wake. J Fluid Mech 264:59–80

    Article  MathSciNet  MATH  Google Scholar 

  • Feng LH, Wang JJ (2010) Circular cylinder vortex-synchronization control with a synthetic jet positioned at the rear stagnation point. J Fluid Mech 662(7):232–259

    Article  MATH  Google Scholar 

  • Gao DL, Chen WL, Li H, Hu H (2017a) Flow around a circular cylinder with slit. Exp Therm Fluid Sci 82:287–301

    Article  Google Scholar 

  • Gao DL, Chen WL, Li H, Hu H (2017b) Flow around a slotted circular cylinder at various angles of attack. Exp Fluids 58(10):1–15

    Article  Google Scholar 

  • Gao DL, Chen GB, Chen WL, Huang YW, Li H (2019a) Effects of steady wake-jets on subcritical cylinder flow. Exp Therm Fluid Sci 102:575–588

    Article  Google Scholar 

  • Gao DL, Huang YW, Chen WL, Chen GB, Li H (2019b) Control of circular cylinder flow via bilateral splitter plates. Phys Fluids 31(5):057105

    Article  Google Scholar 

  • Gao DL, Zhang S, Ning Z, Chen WL, Li H (2021) On the coupling mechanism of rain–wind two-phase flow induced cable vibration: a wake-dynamics perspective. Phys Fluids 33(11):117102

    Article  Google Scholar 

  • Gao DL, Chen GB, Min XW, Chen WL (2022) Wake-vortex evolution behind a fixed circular cylinder with symmetric jets. Exp Therm Fluid Sci 135:110629

    Article  Google Scholar 

  • Gong P, Aju EJ, Jin Y (2022) On the aerodynamic loads and flow statistics of airfoil with deformable vortex generators. Phys Fluids 34:067106

    Article  Google Scholar 

  • Huang Y, He X, Zou Y et al (2021) Pressure distribution, aerodynamic forces and wake-vortex evolution of a sectional cable model controlled with steady windward-and-leeward jets. J vis 24:1155–1172

    Article  Google Scholar 

  • Liang S, Wang J, Xu B, Wu W, Lin K (2018) Vortex-induced vibration and structure instability for a circular cylinder with flexible splitter plates. J Wind Eng Ind Aerodyn 174:200–209

    Article  Google Scholar 

  • Liu YG, Feng LH (2015) Suppression of lift fluctuations on a circular cylinder by inducing the symmetric vortex shedding mode. J Fluids Struct 54:743–759

    Article  Google Scholar 

  • Ma CH, Zhao WW, Wan DC (2022) Numerical investigations of the flow-induced vibration of a three-dimensional circular cylinder with various symmetric strips attached. Phys Fluids 34:065102

    Article  Google Scholar 

  • Mao Q, Zhao J, Liu Y, Sung HJ (2022) Drag reduction by a rotationally oscillating cylinder with a flexible filament. Phys Fluids 34(4):041910

    Article  Google Scholar 

  • Mei YF, Zheng C, Aubry N, Li MG, Wu WT, Liu XL (2021) Active control for enhancing vortex induced vibration of a circular cylinder based on deep reinforcement learning. Phys Fluids 33(10):103604

    Article  Google Scholar 

  • Meng H, Chen WL, Chen GB, Gao DL, Li H (2022) Characteristics of forced flow past a square cylinder with steady suction at leading-edge corners. Phys Fluids 34(2):025119

    Article  Google Scholar 

  • Mishra A, De A (2021) Suppression of vortex shedding using a slit through the circular cylinder at low Reynolds number. Eur J Mech B Fluid 89:349–366

    Article  MathSciNet  MATH  Google Scholar 

  • Mittal C, Sharma A (2021) Flow-induced vibration of a flexible splitter-plate in the wake of a stationary cylinder. Phys Fluids 33(11):113607

    Article  Google Scholar 

  • Modi VJ (1997) Moving surface boundary-layer control: a review. J Fluid Struct 11(6):627–663

    Article  Google Scholar 

  • Nili-Ahmadabadi M, Nematollahi O, Fatehi M et al (2020) Evaluation of aerodynamic performance enhancement of Risø_B1 airfoil with an optimized cavity by PIV measurement. J vis 23:591–603

    Article  Google Scholar 

  • Oruç V (2012) Passive control of flow structures around a circular cylinder by using screen. J Fluids Struct 33:229–242

    Article  Google Scholar 

  • Owen JC, Bearman PW, Szewczyk AA (2001) Passive control of VIV with drag reduction. J Fluids Struct 15(3):597–605

    Article  Google Scholar 

  • Ran Y, Deng Z, Yu H et al (2022) Review of passive control of flow past a circular cylinder. J vis 25:1

    Google Scholar 

  • Wang R, Xin D, Ou J (2019) Experimental investigation on suppressing circular cylinder VIV by a flow control method based on passive vortex generators. J Wind Eng Ind Aerodyn 187:36–47

    Article  Google Scholar 

  • Wu CJ, Wang L, Wu JZ (2007) Suppression of the von karman vortex street behind a circular cylinder by a travelling wave generated by a flexible surface. J Fluid Mech 574(574):365–391

    Article  MathSciNet  MATH  Google Scholar 

  • Yang W, Huang Y, Gao D et al (2021) Ludwig Prandtl’s envisage: elimination of von Kármán vortex street with boundary-layer suction. J vis 24:237–250

    Article  Google Scholar 

  • Zhou B, Wang X, Guo W, Gho WM, Tan SK (2015) Control of flow past a dimpled circular cylinder. Exp Therm Fluid Sci 69:19–26

    Article  Google Scholar 

Download references

Acknowledgements

This research work is supported by the National Natural Science Foundation of China (51978222 and U2106222). This work was also supported by the National Research Foundation of Korea (NRF) grant, which is funded by the Korean government (MSIT) (No. 2020R1A5A8018822, No. 2021R1A2C2012469).

Author information

Authors and Affiliations

Authors

Corresponding authors

Correspondence to Seungho Kim or Wen-Li Chen.

Additional information

Publisher's Note

Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Rights and permissions

Springer Nature or its licensor (e.g. a society or other partner) holds exclusive rights to this article under a publishing agreement with the author(s) or other rightsholder(s); author self-archiving of the accepted manuscript version of this article is solely governed by the terms of such publishing agreement and applicable law.

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Chen, G., Shahsavari, A., Hosseini, S. et al. Wake flow evolution behind a circular cylinder with two perpendicular slits at various angles of attack. J Vis 26, 1233–1246 (2023). https://doi.org/10.1007/s12650-023-00934-2

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s12650-023-00934-2

Keywords

Navigation