TY - GEN
T1 - The oscillatory suction actuator
T2 - AIAA AVIATION 2020 FORUM
AU - Mizrahi, Bar
AU - Seifert, Avraham Avi
N1 - Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - An experimental study of a new oscillatory suction actuator with no moving parts was conducted, for active flow control applications. Following the SaOB (Steady Suction and Oscillatory Blowing) actuator, a new actuator was developed with the ability to create both oscillatory suction and oscillatory blowing. The investigation was conducted in three steps – a benchtop characterization in still-air, actuation-transitional boundary layer interaction over a flat-plate in a small-scale low-speed wind tunnel and implementation on a specially designed airfoil which was tested in a medium-scale wind tunnel. The actuator concept is based on pulsing a pair of ejectors by a single fluidic oscillator. The results show an increase in the actuation efficiency in comparison to steady suction, resulting from a lower energy consumption that leads to the same desired airfoil performance. Lower values of momentum thickness, θ, (points on the ability to delay boundary layer separation) are also achieved by the unsteady suction in comparison to the steady suction.
AB - An experimental study of a new oscillatory suction actuator with no moving parts was conducted, for active flow control applications. Following the SaOB (Steady Suction and Oscillatory Blowing) actuator, a new actuator was developed with the ability to create both oscillatory suction and oscillatory blowing. The investigation was conducted in three steps – a benchtop characterization in still-air, actuation-transitional boundary layer interaction over a flat-plate in a small-scale low-speed wind tunnel and implementation on a specially designed airfoil which was tested in a medium-scale wind tunnel. The actuator concept is based on pulsing a pair of ejectors by a single fluidic oscillator. The results show an increase in the actuation efficiency in comparison to steady suction, resulting from a lower energy consumption that leads to the same desired airfoil performance. Lower values of momentum thickness, θ, (points on the ability to delay boundary layer separation) are also achieved by the unsteady suction in comparison to the steady suction.
UR - http://www.scopus.com/inward/record.url?scp=85092761234&partnerID=8YFLogxK
U2 - 10.2514/6.2020-2941
DO - 10.2514/6.2020-2941
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AN - SCOPUS:85092761234
SN - 9781624105982
T3 - AIAA AVIATION 2020 FORUM
BT - AIAA AVIATION 2020 FORUM
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
Y2 - 15 June 2020 through 19 June 2020
ER -