TY - JOUR
T1 - Active boundary layer tripping using oscillatory vorticity generator
AU - Yehoshua, Tal
AU - Seifert, Avi
N1 - Funding Information:
Partial funding by the Israeli Science Foundation – equipment initiation fund is acknowledged.
PY - 2006/4
Y1 - 2006/4
N2 - The evolution of a train of vortex pairs ejected from a zero-net-mass-flux excitation slot into a Blasius boundary layer was studied experimentally, with the aim of active boundary layer tripping. The excitation was directed upstream or downstream, at a shallow angle, or perpendicular to the surface. Vorticity, circulation, trajectories and convection speeds were calculated and used to describe the vortices' evolution. Intermittency, spectra and mean velocity profiles of the forced boundary layer were measured, in addition to the PIV data. It was found that periodic excitation is very effective for promoting sub-critical transition. More effective, abrupt, boundary layer tripping was identified when the excitation was directed upstream at shallow angle to the surface.
AB - The evolution of a train of vortex pairs ejected from a zero-net-mass-flux excitation slot into a Blasius boundary layer was studied experimentally, with the aim of active boundary layer tripping. The excitation was directed upstream or downstream, at a shallow angle, or perpendicular to the surface. Vorticity, circulation, trajectories and convection speeds were calculated and used to describe the vortices' evolution. Intermittency, spectra and mean velocity profiles of the forced boundary layer were measured, in addition to the PIV data. It was found that periodic excitation is very effective for promoting sub-critical transition. More effective, abrupt, boundary layer tripping was identified when the excitation was directed upstream at shallow angle to the surface.
KW - Actuators
KW - Flow control
KW - Laminar boundary layer
KW - Oscillatory vorticity generators
KW - Transition
KW - Turbulence
UR - http://www.scopus.com/inward/record.url?scp=33645968713&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2005.10.007
DO - 10.1016/j.ast.2005.10.007
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AN - SCOPUS:33645968713
SN - 1270-9638
VL - 10
SP - 175
EP - 180
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
IS - 3
ER -