Experimental Investigations of Different Loudspeakers Applied as Synthetic Jet Actuators

The paper presents the preliminary results of experimental investigation four various loudspeakers used for driving synthetic jet actuator. parameters, characteristic velocity, pressure inside cavity, device sound level (SPL), and heat sink thermal resistance, were presented input power frequency. resonance frequency was determined based on electrical impedance. highest momentum velocity achieved at diaphragm maximum observed, also resonant For same real delivered to actuator its frequency, resistance had lowest value specific loudspeaker. In turn, reached this all actuators tested, dependent velocity.