An experimental study is performed to analyze flow structures behind local
suction and blowing in a flat-plate turbulent boundary layer. The local for
cing is given to the boundary layer flow by means of a sinusoidally oscilla
ting jet issuing from a thin spanwise slot at the wall. The Reynolds number
based on the momentum thickness is about Re-0 = 1700. The effects of local
forcing are scrutinized by altering the forcing frequency (0.011 less than
or equal to f(+) less than or equal to 0.044). The forcing amplitude is fi
xed at A(0) = 0.4. It is found that a small local forcing reduces the skin
friction and the skin friction reduction increases with the forcing frequen
cy. A phase-averaging technique is employed to capture the large-scale vort
ex evolution. An organized spanwise vortical structure is generated by the
local forcing. The cross-sectional area of vortex and the time fraction of
vortex are examined by changing the forcing frequency. An investigation of
the random fluctuation components reveals that turbulent energy is concentr
ated near the center of vortical structures.