TY - GEN
T1 - Wind loads and control of flexible structures embedded in a turbulent boundary layer
AU - Friedland, Ori
AU - Troshin, Victor
AU - Seifert, Avraham
PY - 2014
Y1 - 2014
N2 - We investigate experimentally the flow around a flexible rectangular thin plate positioned normal to the wind direction and embedded in a thick turbulent boundary layer. The purpose of the study is to reduce the plate oscillations caused by unsteady wind loads. Two methods were tested. First we used two mechanical Piezo-electric actuators attached to the plate while the second method used three mass-less Piezo-electric fluidic actuators. The two methods were applied with similar closed-loop control principles: Strain Gauge (SG) sensors captured the plate's oscillations and a simple phase-lag and gain was used to attenuate the oscillations. The results show a reduction of 20-30% of the plate oscillation compared to the uncontrolled case, while a similar increase is possible. The fluidic control was found to be superior to the mechanical control for the current application and conditions. Hypothesized flow physics mechanism link the unsteady pressures created over the plate by actuation to its oscillations.
AB - We investigate experimentally the flow around a flexible rectangular thin plate positioned normal to the wind direction and embedded in a thick turbulent boundary layer. The purpose of the study is to reduce the plate oscillations caused by unsteady wind loads. Two methods were tested. First we used two mechanical Piezo-electric actuators attached to the plate while the second method used three mass-less Piezo-electric fluidic actuators. The two methods were applied with similar closed-loop control principles: Strain Gauge (SG) sensors captured the plate's oscillations and a simple phase-lag and gain was used to attenuate the oscillations. The results show a reduction of 20-30% of the plate oscillation compared to the uncontrolled case, while a similar increase is possible. The fluidic control was found to be superior to the mechanical control for the current application and conditions. Hypothesized flow physics mechanism link the unsteady pressures created over the plate by actuation to its oscillations.
UR - http://www.scopus.com/inward/record.url?scp=84904613182&partnerID=8YFLogxK
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AN - SCOPUS:84904613182
SN - 9781632662651
T3 - 54th Israel Annual Conference on Aerospace Sciences 2014
SP - 1471
EP - 1485
BT - 54th Israel Annual Conference on Aerospace Sciences 2014
PB - Technion Israel Institute of Technology
T2 - 54th Israel Annual Conference on Aerospace Sciences, IACAS 2014
Y2 - 19 February 2014 through 20 February 2014
ER -