Among various devices used in active flow control, plasma synthetic jet actuators seem to be a promising technology to improve aircraft performances. This paper presents a new physical model able to predict the temporal evolution of the main thermodynamic variables of the device. Results for both single pulse mode and repetitive working regime are reported, providing insights of their characteristics. The work is completed by an analysis of the actuator frequency response, followed by a comparison with literature results.
Development of a physical model for plasma synthetic jet actuators / Chiatto, Matteo; Palumbo, Andrea; DE LUCA, Luigi. - (2015), pp. 1-10. (Intervento presentato al convegno XXII Congresso Associazione Italiana di Meccanica Teorica e Applicata tenutosi a Genova nel 14-17/09/2015).
Development of a physical model for plasma synthetic jet actuators
CHIATTO, MATTEO;PALUMBO, ANDREA;DE LUCA, LUIGI
2015
Abstract
Among various devices used in active flow control, plasma synthetic jet actuators seem to be a promising technology to improve aircraft performances. This paper presents a new physical model able to predict the temporal evolution of the main thermodynamic variables of the device. Results for both single pulse mode and repetitive working regime are reported, providing insights of their characteristics. The work is completed by an analysis of the actuator frequency response, followed by a comparison with literature results.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
