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Experiments on three-dimensional wall-layer scale Lorentz actuators in high-Reynolds-number axisymmetric turbulent boundary layers
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10.1063/1.2887983
/content/aip/journal/pof2/20/3/10.1063/1.2887983
http://aip.metastore.ingenta.com/content/aip/journal/pof2/20/3/10.1063/1.2887983

Figures

Image of FIG. 1.
FIG. 1.

Schematic diagram of the electrode-magnet array in two-dimensional actuators for producing large scale cross-stream body force and secondary flow. The solid curved lines between the magnet pairs indicate the permanent magnetic field lines . The broken curved lines with the pairs of arrows between the electrode pairs indicate the pulsating applied electric current density field lines .

Image of FIG. 2.
FIG. 2.

Schematic top view of the electrode and magnet configuration in the present three-dimensional actuator (also see Fig. 3). The widths of the electrodes and the magnets are each; the gaps between the neighboring electrodes and magnets are and , respectively. The magnets are long. The electrodes are plated onto a plastic (kapton) sheet, which is screwed to and held taut by two axial bus bars (see Fig. 3)—positive and negative—each wide, located diametrically opposite to each other. At a freestream velocity of , is 176 wall units. The inner boundary of the actuator is 528 and 1056 wall units in the spanwise and streamwise directions, respectively. The solid lines between the magnet pairs indicate the permanent magnetic field lines . The pair of broken lines between the electrode pairs indicates the pulsating applied electric current density field lines .

Image of FIG. 3.
FIG. 3.

The experimental model. (a) A scaled drawing of one quarter length of the floating section of the axisymmetric model is shown. The floating cylinder is populated with three-dimensional actuators shown in Fig. 2. The electrodes run azimuthally with the north and the south poles lying in between. The inner cutout in (a) shows the steel rings under the magnets. The four screws per quarter length of the floating cylinder are visible on the right in (a) over the bus bar. They help align and hold down the kapton sheet of the electrodes over the magnets. The actuator dimension best matched one unit turbulence production domain at . (b) Photograph of the entire axisymmetric model and the sting support (on left).

Image of FIG. 4.
FIG. 4.

Schematic of the axisymmetric experimental model showing the location of the floating electromagnetic actuator section and the boundary layer trip. The stainless steel tube sting support passes through the entire model, which is hollow, through the tail end on right [see Fig. 3(b)].

Image of FIG. 5.
FIG. 5.

Laser Doppler measurements (symbols) of the mean velocity profile at the downstream end of the floating section in wall layer scales when the actuators have been turned off. The solid line is a smooth flat-wall log law .

Image of FIG. 6.
FIG. 6.

Laser Doppler measurements (symbols) of the streamwise turbulence profile at the downstream end of the cylindrical floating section when actuators have been turned off compared with flat-plate zero-pressure-gradient measurements due to Klebanoff (Ref. 39) (solid line; Reynolds number of ) and Purtell et al. (Ref. 37) (broken lines, which show the upper and lower bounds of data in the range of Reynolds numbers from 485 to 5100).

Image of FIG. 7.
FIG. 7.

Laser Doppler measurements (symbols) of the surface-normal turbulence profile at the downstream end of the floating section when actuators have been turned off compared with the measurements due to Klebanoff (Ref. 39) (solid line, ).

Image of FIG. 8.
FIG. 8.

Reynolds number dependence of the efficiency of drag reduction in two-dimensional and three-dimensional actuators. Filled diamonds and squares are from channel flow measurements in Ref. 16 at and 418 (defined with half channel height and ), respectively. Cut X symbols are DNS data in turbulent boundary layers at from Ref. 18. Triangles and x symbols are the DNS data (Ref. 18) scaled to Reynolds numbers of 289 and 418, respectively. The solid and broken lines are least-square linear fits. Open circles are present data on three-dimensional actuators in turbulent boundary layers over axisymmetric bodies at .

Image of FIG. 9.
FIG. 9.

Comparison of drag reduction between two- and three-dimensional actuators in turbulent boundary layers. The value of is 1.0 in two-dimensional actuators and is taken to be 0 in the present three-dimensional actuators. Filled diamonds: present work on axisymmetric bodies with numerous three-dimensional actuators at . Open circles are measurements due to Pang and Choi (Ref. 17) at . Plus symbols are DNSs due to Berger et al. (Ref. 18) at . Solid line is a trend line due to Pang and Choi (Ref. 17) drawn through theirs and Berger et al.’s (Ref. 18) two-dimensional actuator data.

Image of FIG. 10.
FIG. 10.

Laser Doppler measurements of the surface-normal turbulence near wall when the electrodes are powered (filled symbol) or not (open symbol). The solid line is a least square third order polynomial fit to the reference (open symbol) data. The pulsing frequency is bipolar, the freestream speed is , the conductivity of the water is , the electrode voltage and currents are and , respectively.

Tables

Generic image for table
Table I.

Lorentz actuators: Summary of experiments reported.

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Table II.

Lorentz actuators: Summary of simulations reported.

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Table III.

Estimates of the frequency of Lorentz pulsing in the present experiments based on bursting frequency and on small-scale local Stokes flow modeling.

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/content/aip/journal/pof2/20/3/10.1063/1.2887983
2008-03-31
2014-04-21
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752b84549af89a08dbdd7fdb8b9568b5 journal.articlezxybnytfddd
Scitation: Experiments on three-dimensional wall-layer scale Lorentz actuators in high-Reynolds-number axisymmetric turbulent boundary layers
http://aip.metastore.ingenta.com/content/aip/journal/pof2/20/3/10.1063/1.2887983
10.1063/1.2887983
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