Hydrodinamic effect of Discharge of Dielectric Barrier in the flow of air around an airfoil NACA 0018

David Alamilla-Flores, Martín Nieto-Peréz, Pedro J. Argumedo-Teuffer

Producción científica: Capítulo del libro/informe/acta de congresoContribución a la conferenciarevisión exhaustiva

Resumen

The presented work is aimed to study the boundary layer re-attachment of flow over an airfoil at high angles of attack. To promote the reattachment, a flat profile with an asymmetric DBD actuator on one of its surfaces was built based on the optimization improvements of the actuator to observe its effect at quiescent flow conditions. Subsequently, asymmetric actuators were tested in streamwise orientation on the upper surface of a NACA 0018 airfoil. The plasma actuators were installed symmetrically between the leading edge and trailing edge of the profile. We have used Schlieren type-z optical arrangement to study the flow induced in atmospheric pressure air by electrohydrodynamic body forces generated by a DBD plasma actuator energized by a radiofrequency power supply. The schlieren images show the absence of significant vertical flow. The electrical parameters of the discharge were generated by a radiofrequency source operating 1-16 Kvpp at a frequency 17-35 KHz.

Idioma originalInglés
Título de la publicación alojada16th Latin American Workshop on Plasma Physics, LAWPP 2017 - Conference Proceedings
EditorialInstitute of Electrical and Electronics Engineers Inc.
Páginas1-4
Número de páginas4
ISBN (versión digital)9781538633861
DOI
EstadoPublicada - 2 jul. 2017
Publicado de forma externa
Evento16th Latin American Workshop on Plasma Physics, LAWPP 2017 - Mexico City, México
Duración: 4 sep. 20178 sep. 2017

Serie de la publicación

Nombre16th Latin American Workshop on Plasma Physics, LAWPP 2017 - Conference Proceedings

Conferencia

Conferencia16th Latin American Workshop on Plasma Physics, LAWPP 2017
País/TerritorioMéxico
CiudadMexico City
Período4/09/178/09/17

Huella

Profundice en los temas de investigación de 'Hydrodinamic effect of Discharge of Dielectric Barrier in the flow of air around an airfoil NACA 0018'. En conjunto forman una huella única.

Citar esto