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Wall pressure fluctuations of a turbulent separated and reattaching flow affected by an unsteady wake
Authors:Sejong?Chun,Ying?Zheng?Liu,Hyung?Jin?Sung  author-information"  >  author-information__contact u-icon-before"  >  mailto:hjsung@kaist.ac.kr"   title="  hjsung@kaist.ac.kr"   itemprop="  email"   data-track="  click"   data-track-action="  Email author"   data-track-label="  "  >Email author
Affiliation:(1) Department of Mechanical Engineering, Korea Advanced Institute of Science and Technology, 373–1 Kuseong-dong Yuseong-gu, 305–701 Daejeon, Korea;(2) School of Mechanical Engineering, Shanghai Jiao Tong University, 1954 Huashan Road, 200030 Shanghai, China
Abstract:The spatio-temporal characteristics of the wall-pressure fluctuations in separated and reattaching flows over a backward-facing step were investigated through pressure-velocity joint measurements carried out using multiple-arrayed microphones and split-film probes. A spoke-wheel-type wake generator was installed upstream of the backward-facing step. The flow structure at the effective forcing frequency (Stf=0.2) was found to be well organized in terms of wall pressure spectrum, cross-correlation, wavenumber-frequency spectrum, and wavelet auto-correlation. Introduction of the unsteady wake (Stf=0.2) reduced the reattachment length by 10%. In addition, the unsteady wake enhanced the turbulence intensity near the separation edge and, as a consequence, enhanced the quadrupole sound sources; however, the turbulence intensity near the reattachment region was weakened and the overall flow noise was attenuated. The greater organization of the flow structure induced by the unsteady wake led to a weakening of the dipole sound sources, which are the dominant sound sources in this system. The dipole sound sources generated by wall pressure fluctuations were calculated using Curlersquos integral formula.Abbreviations AR Aspect ratio - SBF Spatial box filteringRoman symbols Cpprime Wall pressure fluctuation coefficient, pprime/0.5rgrUinfin2 - H Step height of backward-facing step (mm) - Hs Shape factor (Hs=delta*/theta) - Rs Distance from acoustic source point to observation point (m) - ReH Reynolds number,UinfinH/ngr - St The reduced frequency,fH/Uinfin - Stf Normalized forcing frequency by unsteady wake, fpH/Uinfin - T Vortex shedding period (s) - Uinfin Free-stream velocity (m/s) - a Speed of sound (m/s) - f Frequency (Hz) - fp Wake passing frequency (Hz) - k Turbulent kinetic energy (m2/s2) - kx Streamwise wave number (1/m) - kz Spanwise wave number (1/m) - lj Cosine of angle - p Instantaneous wall pressure (Pa) - prms Root-mean-square of wall pressure (Pa) - pSBF Spatial box filtered wall pressure (Pa) - pd Dipole sound source (Pa) - pw Conditionally-averaged wall pressure (Pa) - q Dynamic pressure, 0.5rgrUinfin2(Pa) - r Distance from origin to observation point (mm) - uc Convection velocity (m/s) - uprimemax Root-mean-square of streamwise velocity (m/s) - xR Time-mean reattachment length (mm)Greek symbols gammap Forward-flow time fraction - $$rho _{{pp}} {left( {Delta t;x_{0} } right)} $$ Auto-correlation of pressure atx0 - $$rho _{{pp}} {left( {xi ,zeta ,Delta t;x_{0} ,z_{0} } right)} $$ Two-dimensional cross-correlation of pressure with streamwise separation interval xgr, spanwise separation interval zeta, and time delay $$Delta t $$, at (x0,z0) - delta Boundary layer thickness (mm,delta99%) - delta* Displacement thickness (mm, $$delta ^{ * } = {int_0^{Y to infty } {{left( {1 - u mathord{left/ {vphantom {u U}} right. kern-nulldelimiterspace} U} right)}{text{d}}y} } $$) - deltaij Kroneckerrsquos delta function - phgr Phase angle (°) - lambda Wavelength (mm) - theta Momentum thickness (mm, $$theta = {int_0^{Y to infty } {{left( {1 - u mathord{left/ {vphantom {u U}} right. kern-nulldelimiterspace} U} right)}u mathord{left/ {vphantom {u U}} right. kern-nulldelimiterspace} U{text{d}}y} } $$) - phiv Angle between vertical axis and observation point (°) - rgr Density (kg/m3) - tau Time delay (s) - xgr Streamwise separation interval (m) - zeta Spanwise separation interval (m) - Fcyp(f;x0) Autospectrum of pressure measured atx0 (Pa2s) - Fcypp(xgr, ohgr;x0) Streamwise cross spectrum of pressure atx0 (Pa2s) - Fcypp(xgr, zeta, ohgr; x0,z0) Streamwise and spanwise cross spectrum of pressure at (x0,z0) (Pa2s) - Fcypp(kx, ohgr; x0) Streamwise wavenumber-frequency spectrum of pressure at x0(Pa2s) - Fcypp(kx, kz, ohgr;x0,z0) Two-dimensional wavenumber-frequency spectrum of pressure at (x0,z0) (Pa2s)
Keywords:Backward-facing step  Unsteady wake  Dipole sound source
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