Abstract
We present the results of an experimental study in which a planar laminar jet of air was forced by an array of micro-electromechanical systems (MEMS) micro-actuators. In the absence of forcing, the velocity profile of the experimental jet matched the classic analytic solution. Driving actuators on either side of the jet in-phase or anti-phase, respectively, excited the symmetric or anti-symmetric mode of instability of the jet. Asymmetric forcing, using MEMS actuators on only one side of the jet, was also investigated.
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Abbreviations
- x, y, z :
-
Streamwise, cross-stream, and spanwise coordinates
- u :
-
Streamwise velocity
- d :
-
Exit slit width
- U 0 :
-
Centerline streamwise velocity
- b :
-
Jet half-width
- v :
-
Kinematic viscosity
- Re :
-
Reynolds number=U 0 b/v
- M :
-
Momentum flux
- δu :
-
Fluctuating velocity component in x direction
- f :
-
Forcing frequency of MEMS actuators
- ω :
-
Dimensionless frequency of velocity fluctuations=fb/U 0
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Peacock, T., Bradley, E., Hertzberg, J. et al. Forcing a planar jet flow using MEMS. Exp Fluids 37, 22–28 (2004). https://doi.org/10.1007/s00348-004-0780-8
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DOI: https://doi.org/10.1007/s00348-004-0780-8