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

Bibliographie
- 206 -
[124] Benard N, Braud P, Pons J, Touchard G et Moreau E, 2007, “Quasi-steady and unsteady
actuatino by surface non-thermal plasma discharge for control of a turbulent round air jet”,
Journal of Turbulence, Vol. 8, pp. 1-24.
[125] List L, Byerley AR, McLaughlin TE et Van Dycken RD, 2003, “Using a plasma actuator to
control laminar separation on a linear cascade turbine blade”, Proc. of the 45 th AIAA
Aerospace Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2003-1026.
[126] Van Dycken RD, Perez-Blancho H, Byerley AR et McLaughlin TE, 2004, “Plasma
actuatorfor wake flow control of high camber blades during part load operation”, Proc. of the
ASME GT2004-53227, Vienna, Austria.
[127] Morris SC, Corke TC, VanNess D, Stephens J et Douville T, 2005, “Tip clearance control
using plasma actuators”, Proc. of the 43 th AIAA Aerospace Sciences Meeting and Exhibit,
Reno, NV, AIAA Paper 2005-0782.
[128] Douville T, Stephens J, Corke TC et Morris SC, 2006, “Turbine blade tip leakage flow
control by partial squealer tip and plasma actuators”, Proc. of the 44 th AIAA Aerospace
Sciences Meeting and Exhibit, Reno, NV, AIAA Paper 2006-20.
[129] Van Ness DK, Corke TC et Morris SC, 2006, “Turbine tip clearance flow control using
plasma actuation”, Proc. of the 44 th AIAA Aerospace Sciences Meeting and Exhibit, Reno,
NV, AIAA Paper 2006-21.
[130] Van Ness DK, Corke TC et Morris SC, 2007, “Stereo PIV of a turbine tip clearance flow
with plasma actuation”, Proc. of the 45 th AIAA Aerospace Sciences Meeting and Exhibit,
Reno, NV, AIAA Paper 2007-647.
[131] Corke TC, Thomas FO et Huang J, 2007, “Documentation and control of flow separation on
a low pressure turbine linear cascade of Pak-B blades using plasma actuators”, NASA
Technical Report, NASA/CR 2007-214677.
[132] Corke TC, Thomas FO et Klapetzky MJ, 2007, “Use of plasma actuators as a moving wake
generator”, NASA Technical Report, NASA/CR 200-214676.
[133] Bonnet JP, 2006, “Bilan EFFC (European Forum on Flow Control 2, mai à juillet 2006 au
LEA”, Proc. du GDR2505 Contrôle des décollements, Toulouse, France.
[134] Siauw WL, Tensi J, Bourgois S, Bonnet JP, Breux JM et Maria I, 2006, “Control of flow
separation and its associated physics on a NACA 0015 using synthetic jet actuators”, Proc.
of the 2 nd ASME Joint U.S.-European Fluids Engineering Summer Meeting: Forum on the
Control of Separated Flow, Miami, FL., FDSEM2006-98519.
[135] Barlow JB, Rae WH et Pope A, 1999, “Low-speed wind tunnel testing”, 3 rd éd.
[136] Sheldahl RE et Klimas PC, 1981, “Aerodynamic characteristics of seven symmetrical airfoil
sections through 180-degree angle of attack for use in aerodynamic analysis of vertical axis
wind turbines”, SANDIA Report, SAND80-2114.
[137] McAlister KW et Takahashi RK, 1991, “NACA 0015 wing pressure and trailing vortex
measurements”, NASA Technical Paper No. 3151.
[138] Abbot IH, von Doenhoff AE et Stivers LS, 1945, “Summary of airfoil data”, NACA Report
No. 824.
[139] Jacobs N et Sherman A, 1937, “Airfoil section characteristics as affected by variations of the
Reynolds number”, NACA Report No. 586.
[140] Bénard N, Braud P, Jolibois J et Moreau E, 2008, “Airflow reattachment along a NACA
0015 airfoil by surface dielectric barrier discharge actuator: Time-resolved particle image
velocimetry investigation”, Proc. of the 4 th AIAA Flow Control Conference, Seattle, WA.,
AIAA Paper 2008-4202.