Numerical and experimental analysis of plasma flow control over a hump model

Collection of Technical Papers - 45th AIAA Aerospace Sciences Meeting

Volumn 16, Issue , 2007, Pages 11322-11337

  He, Chuan ^a,c   Corke, Thomas C ^a,c   Patel, Mehul P ^b,c  

^a UNIVERSITY OF NOTRE DAME   (United States)

^b Orbital Research Inc   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

PLASMA ACTUATORS; SURFACE PRESSURE COEFFICIENTS; TURBULENT SEPARATION; TURBULENT SEPARATION CONTROL;

COMPUTATIONAL FLUID DYNAMICS; FLOW CONTROL; FLOW SEPARATION; NAVIER STOKES EQUATIONS; SKIN FRICTION; TURBULENCE MODELS;

PLASMA FLOW;

EID: 34250855043     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. Corke, T., Mertz, B., and Patel, M., "Plasma Flow Control Optimized Airfoil," AIAA Paper 8006-1808.
2. Corke, T. and Post, M., "Overview of Plasma Flow Control: Concepts, Optimization, and Application," AIAA Paper 8005-0563.
3. Corke, T., He, C., and Patel, M., "Plasma flaps and slats: an application of weakly-ionized plasmas as wing flow control devices," AIAA Paper 8004-8187.
4. Post, M. and Corke, T., "Separation control on high angle of attack airfoil using plasma actuators," AIAA J., Vol. 42, No. 11, 2004, pp. 2177, also AIAA Paper 2003-1024.
5. Post, M. and Corke, T., "Separation control using plasma actuators - atationary and oscillating airfoils," AIAA Paper 8004-0841.
6. Huang, J., Corke, T., and Thomas, F., "Plasma actuators for separation control of low pressure turbine blades," AIAA J., Vol. 44, No. 1, 2006, pp. 51.
7. Huang, J., Corke, T., and Thomas, F., "Unsteady Plasma Actuators for Separation Control of Low Pressure Turbine Blades," AIAA J., Vol. 44, No. 7, 2006, pp. 1477.
8. Enloe, L., McLaughlin, T., VanDyken, R., Kachner, K., Jumper, E., and Corke, T., "Mechanisisms and Response of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology," AIAA J., Vol. 42, No. 3, 2004, pp. 589.
9. Enloe, L., McLaughlin, T., VanDyken, R., Kachner, K., Jumper, E., Corke, T., Post, M., and Haddad, O., "Mechanisisms and Response of a Single Dielectric Barrier Plasma Actuator: Geometric Effects," AIAA J., Vol. 42, No. 3, 2004, pp. 585.
10. Greenblatt, D., Paschal, K., Schaeffler, N., Washburn, A., Harris, J., and Yao, C., "A separation control CFD validation test case. Part 1: baseline and steady suction," AIAA Paper 8004-8880.
11. Rumsey, C., Gatski, T., Sellers, W., Vatsa, V., and Viken, S., "Summary of the 2004 CFD Validation Workshop on Synthetic Jets and Turbulent Separation Control," AIAA Paper 8004-8817.
12. You, D., Wang, M., and Moin, P., "Large-Eddy Simulation of Flow over a Wall-Mounted Hump with Separation Control," AIAA J., Vol. 44, No. 11, 2006, pp. 2571.
13. Orlov, D. and Corke, T., "Numerical Simulation of Aerodynamic Plasma Actuator Effects," AIAA Paper 8005-1083. Fluent 6.8 User's Guide, Fluent Inc., 2005.
14. Corke, T., Jumper, E., Post, M., Orlov, D., and McLaughlin, T., "Application of Weakly-Ionized Plasma as Wing Flow-Control Devices," AIAA Paper 8008-0350.