Etude et développement d'un actionneur plasma à décharge à ...

Bibliographie
[73] Moreau E, Léger L et Touchard G, 2006, “Effect of a DC surface-corona discharge on a flat
plate boundary layer for airflow velocity up to 25 m/s”, Journal of Electrostatics, Vol. 64,
No. 3-4, pp. 215-225.
[74] Laurentie JC, 2008, “Actionneurs plasmas pour le contrôle des écoulements – Étude du
courant de décharge et optimisation de la conversion électromécanique”, Rapport de Master
2, Univ. Poitiers.
[75] Pons J, Moreau E et Touchard G, 2007, “Electrohydrodynamic properties of surface
dielectric barrier discharge in ambient air for aerodynamic airflow control”, Proc. of the 28 th
ICPIG, Prague, Czech Republic.
[76] Forte M, 2007, “Contrôle d’écoulement par actionneur plasma de type Décharge à Barrière
Diélectrique – Application à l’amélioration de la pulvérisation dans les injecteurs de
turboréacteurs”, Thèse Univ. Poitiers.
[77] Forte M, Jolibois J, Pons J, Moreau M, Touchard G et Cazalens M, 2007, “Optimization of a
dielectric barrier discharge actuator by stationary and non-stationary measurements of the
induced flow velocity: application to airflow control”, Exp. in Fluids, Vol. 43, pp. 917 – 928.
[78] Roth JR et Dai X, 2006, “Optimization of the aerodynamic plasma actuator as an
Electrohydrodynamic (EHD) electrical device”, Proc. of the 44 th AIAA Aerospace Sciences
Meeting and Exhibit, Reno, NV, AIAA Paper 2006-1203.
[79] Enloe CL, McLaughlin TE et Font GI, 2005, “Parametrization of temporal structure in the
single dielectric barrier aerodynamic plasma actuator”, Proc. of the 43 th AIAA Aerospace
Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2005-564.
[80] Dong B, Bauchire JM, Pouvesle JM, Magnier P et Hong D, 2008, “Experimental study of a
DBD surface discharge for the active control of subsonic airflow”, J. Phys. D: Appl. Phys.,
Vol. 41, No. 15, 155201 (9 pp).
[81] http://www.goodfellow.com/home.aspx?LangType=1036
[82] Abe T, Takizawa Y, Sato S et Kimura N, 2007, “A parametric experiemental study for
momentum transfer by plasma actuator”, Proc. of the 45 th AIAA Aerospace Sciences
Meeting and Exhibit, Reno, NV, AIAA Paper 2007-187.
[83] Takizawa Y, Matsuda A, Kikuchi K, Sasoh A et Abe T, 2007, “Optical observation of
discharge plasma structure in DBD plasma actuator”, Proc. of the 38 th AIAA
Plasmadynamics and Lasers Conference, Miami, FL, AIAA Paper 2007-4376.
[84] Lagmich Y, 2007, “Diagnostique et modélisation d’une décharge à barrière diélectrique pour
le contrôle d’écoulement”, Thèse Univ. Toulouse.
[85] Gibalov VI et Pietsch GJ, 2000, “The development of dielectric barrier discharges in gas
gaps and on surfaces”, J. Phys. D: Appl. Phys., Vol. 33, pp. 2618-2636.
[86] Font GI, Enloe CL, McLaughlin TE et Orlov D, 2007, “Plasma discharge characteristics and
experimentally determined boundary conditions for a plasma actuator”, Proc. of the 45 th
AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2007-188.
[87] Enloe CL, McLaughlin TE, Gregory JW, Medina RA et Miller WS, 2008, “Surface potential
and electric field structure in the aerodynamic plasma actuator”, Proc. of the 46 th AIAA
Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2008-1103.
[88] Prandtl L, 1904, “Uber flussigkeitsbewegung bei sehr kleiner reibung”, Internationaler
Mathematiker-Kongress Heidelberg, Vol. Verhandlungen 3, pp. 484-491.
[89] Reynols O, 1883, “An experimental investigation of the circumstances which determine
whether the motion of the water shall be direct or sinous, and of the law of resistance in
parallel channels”, Proc. of the Royal Society of London, Vol. 35, pp. 84-99.
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