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Active control of flow noise sources in turbulent boundary layer on a flat-plate using piezoelectric bimorph film

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Abstract

The piezoelectric bimorph film, which, as an actuator, can generate more effective displacement than the usual PVDF film, is used to control the turbulent boundary-layer flow. The change of wall pressures inside the turbulent boundary layer is observed by using the multi-channel microphone array flush-mounted on the surface when actuation at the non-dimensional frequency f +b =0.008 and 0.028 is applied to the turbulent boundary layer. The wall pressure characteristics by the actuation to produce local displacement are more dominantly influenced by the size of the actuator module than the actuation frequency. The movement of large-scale turbulent structures to the upper layer is found to be the main mechanism of the reduction in the wallpressure energy spectrum when the 700v/uτ-long bimorph film is periodically actuated at the non-dimensional frequency f +b =0.008 and 0.028. The biomorph actuator is triggered with the time delay for the active forcing at a single frequency when a 1/8″ pressuretype, pin-holed microphone sensor detects the large-amplitude pressure event by the turbulent spot. The wall-pressure energy in the late-transitional boundary layer is partially reduced near the convection wavenumber by the open-loop control based on the large amplitude event.

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Abbreviations

Δx+ :

Normalized streamwise length (≡ uτΔx/v)

Δz+ :

Normalized spanwise length (≡ uτΔz/v)

f +b :

Mean bursting frequency (≡ fv/u 2τ

U0 :

Flow velocity

Uc :

Convective velocity

Uτ :

Friction velocity

v:

Viscosity

d+ :

Non-dimensional pin-hole diameter (≡ uτd/v)

Reθ :

Reynolds number based on momentum thickness

kx :

Streamwise wavenumber (rad/m)

τω :

Mean wall shear-stress

References

  • Abraham, B. M. and Keith, W. L., 1998, “Direct Measurements of Turbulent Boundary Layer Wall Pressure Wavenumber-Frequency Spectra,”ASME J. Fluids Eng., Vol. 20, pp. 29–39.

    Article  Google Scholar 

  • Blackwelder, R. F. and Haritonidis, J. H., 1983, “Scaling of the Bursting Frequency in Turbulent Layers,”J. Fluid Mech., Vol. 132, pp. 87–103.

    Article  Google Scholar 

  • Choi, H. and Moin, P., 1990, “On the Space-Time Characteristics of Wall-Pressure Fluctuations,”physics of Fluids A, Vol. 2, pp. 1450–1460.

    Article  Google Scholar 

  • Collis, S. S., Joslin, R. D., Seifert, A. and Theofilis, V., 2004, “Issues in Active Flow Control: theory, control, simulation and experiment,”Progress in Aerospace Sciences, Vol. 40, pp. 237–289.

    Article  Google Scholar 

  • Farabee, T. M. and Casarella, M. J., 1991, “Spectral Features of Wall Pressure Fluctuations Beneath Turbulent Boundary Layers,”physics of Fluids A, Vol. 3, pp. 2410–2420.

    Article  Google Scholar 

  • Gad-el-Hak, M., 2000, Flow Control, Cambridge University Press.

  • Jacobson, S. A. and Reynolds, W. C., 1998, “Active Control of Streamwise Vortices and Streaks in Boundary Layers,”J. Fluid Mech., Vol. 360, pp. 179–211.

    Article  MATH  Google Scholar 

  • Jeon, W. -P. and Blackwelder, R. F., 2000, “Perturbations in the Wall Region Using Flush Mounted Piezoceramic Actuators,”Exps. Fluids, Vol. 28, No. 6, pp. 485–496.

    Article  Google Scholar 

  • Keith, W. L. and Bennett, J. C., 1991, “Low Frequency Measurements of the Wall Shear Stress and Wall Pressure in a Turbulent Boundary Layer,”AIAA, Vol. 29, No. 4, pp. 526–530.

    Article  Google Scholar 

  • Landahl, M. T., 1975, “Wave Mechanics of Boundary Layer Turbulence Layer,”J.A.S.A., Vol. 57, pp. 824–831

    Google Scholar 

  • Lee, S. and Kim, H.-J., 1999, “Experimental Study on Wall Pressure Fluctuations in the Turbulent Boundary Layer on a Flat-Plate,”J. KSME, Part B, 23, No. 6, pp. 722–733.(in Korean)

    Google Scholar 

  • Powell, A., 1960, “Aerodynamic Noise and the Plane Boundary,”J.A.S.A., Vol. 32, pp. 982–990

    MathSciNet  Google Scholar 

  • Smith, B. L. and Glezer, A., 1998, “The Formation and Evolution of Synthetic Jets,”physics of Fluids, Vol. 10, pp. 2281–2297.

    Article  MATH  MathSciNet  Google Scholar 

  • Wang, M., Lele, S. K., Moin, P., 1996, “Sound Radiation during Local Breakdown in a low Mach-number Boundary Layer,”J. Fluid Mech., Vol. 319, pp. 311–328

    Article  Google Scholar 

  • Wehrmann, O. H., 1965, “Reduction of Velocity Fluctuations in a K’arm’an Vortex Street by Vibrating Cylinder,”physics of Fluids, Vol. 8, pp. 760–761.

    Article  Google Scholar 

  • Wehrmann, O. H., 1967, “Self-Adjusting Feedback Loop for Mechanical Systems to Influence Flow in Transition. Part I,” Boeing Scientific Research Lab., Document D1-82-0632.

  • Wiltse, J. M. and Glezer, A., 1993, “Manipulation of Free Shear Flows Using Piezoelectric Actuators,”J. Fluid Mech., Vol. 249, pp. 261–285.

    Article  Google Scholar 

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Correspondence to Seungbae Lee.

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Song, WS., Lee, S., Shin, DS. et al. Active control of flow noise sources in turbulent boundary layer on a flat-plate using piezoelectric bimorph film. J Mech Sci Technol 20, 1993–2001 (2006). https://doi.org/10.1007/BF03027592

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  • DOI: https://doi.org/10.1007/BF03027592

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