Wall normal jet under elevated temperatures produced by surface plasma actuator

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 14, Issue , 2007, Pages 9611-9618

  Segawa, Takehiko ^a,c,d   Furutani, Hirohide ^a,c   Yoshida, Hiro ^a,c   Jukes, Timothy ^b,d   Choi, Kwing So ^b,d  

^a NATIONAL INSTITUTE OF ADVANCED INDUSTRIAL SCIENCE AND TECHNOLOGY AIST   (Japan)

^b UNIVERSITY OF NOTTINGHAM   (United Kingdom)

^c Energy Technology Institute   (Japan)

^d AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ALUMINA; DIELECTRIC MATERIALS; FLOW VISUALIZATION; GLASS; HIGH TEMPERATURE EFFECTS; PHOTOGRAPHY; PLASMA DEVICES; QUARTZ;

DIELECTRIC BARRIER DISCHARGE (DBD); PLASMA ACTUATORS; SCHLIEREN PHOTOGRAPHY SYSTEMS;

JET AIRCRAFT;

EID: 34250835014     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-784     Document Type: Conference Paper

References (10)

1. Roth, J. R., Sherman, D. M., and Wilkinson, S. P. (1998). Boundary layer flow control with a one atmosphere uniform glow discharge. AIAA Paper 98-0328, 36th Aerospace Sciences Meeting and Exhibit, Reno, Nevada.
2. Roth, J. R., Mohan R.C.M., Yadav, M., Rahel, J., and Wilkinson S. P. (2004). Flow field measurements of paraelectric, peristaltic and combined plasma actuators based on the one Atmospheric uniform glow discharge plasma (OAUGDP™). AIAA Paper 2004-0845, 42nd Aerospace Sciences Meeting and Exhibit, Reno, Nevada.
3. Corke, T. C., Jumper, E. J., Post, M. L., Orlov, D., and McLaughlin, T. E. (2002). Application of weakly-ionized plasmas as wing flow-control devices. AIAA paper 2002-0350, 40th Aerospace Sciences Meeting & Exhibit, Reno, Nevada.
4. Jayaraman, B. and Shyy, W. (2003). Flow Control and thermal management using dielectric glow discharge concepts. AIAA Paper 2003-3712, 33rd Fluid Dynamics Conference, Orlando, Florida.
5. VanDyken, B., Perez-Blanco, H., Mclaughlin, T., and Byerley, A. (2005). Turbine cascade flow control using a "wake filling" pulsed plasma actuator. GT2005-68114, ASME TURBO EXPO 2005, Reno, Nevada.
6. Jukes, T., Choi, K-S., Scott, S., and Johnson, G. (2006). Turbulent drag reduction by surface plasma through spanwise flow oscillation. AIAA Paper 2006-3693, 3rd Flow Control Conference, San Francisco, California.
7. Shyy, W., Jayaraman, B., Andersson, A., "Modeling of glow discharge-induced fluid dynamics," Journal of Applied Physics, Vol. 92, No. 11, 2002, pp. 6434-6443.
8. Roy, S. and Gaitonde, D. V. (2005). Modeling surface discharge effects of atmospheric RF on gas flow control. AIAA 2005-160, 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada.
9. Segawa, T., Jukes, T., and Choi, K-S, private communication, "Flow visualization of wall normal jet using surface plasma actuator with circular electrode", Regular Meeting on Active Turbulence Control, Faculty of Engineering, University of Nottingham, February, 2005.
10. Santhanakrishnan, A. and Jacob, J. D. (2006). On plasma synthetic jet actuators. AIAA paper 2006-0317, 44th Aerospace Sciences Meeting, Reno, Nevada.