Paper
24 August 2000 Piezoelectric actuator for pulsating jets
Michel Brissaud, Paul Gonnard, Jean-Christophe Bera, Michel Sunyach
Author Affiliations +
Abstract
Recent researches in aeronautics showed that fluidic actuator systems could offer possibilities for drag reduction and lift improvement. To this end many actuator types were designed. This paper deals with the design, fabrication and test of piezoelectric actuator in order to generate pulsated jets normal to a surface and control air flow separation. It is based on the flexural displacement of a rectangular metal plate clamped on one of its large edge. Piezoelectric patches cemented on the plate were used for driving into vibration the actuator. Experimental measurements show that pulsed flow velocities are adjustable from 1.5m/s to 35m/s through a 100x1mm2 slit andwithin a 100 to 400 Hz frequency range. Prototype provides the jet performances classically required for active control flow.
© (2000) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Michel Brissaud, Paul Gonnard, Jean-Christophe Bera, and Michel Sunyach "Piezoelectric actuator for pulsating jets", Proc. SPIE 4073, Fifth European Conference on Smart Structures and Materials, (24 August 2000); https://doi.org/10.1117/12.396418
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CITATIONS
Cited by 3 scholarly publications.
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KEYWORDS
Actuators

Finite element methods

Velocity measurements

Metals

Visualization

Aerodynamics

Control systems

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