Numerical study of shockwave induced boundary layer separation control using plasma actuators

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Kalra, Chiranjeev S ^a   Shneider, Mikhail N ^a   Miles, Richard B ^a  

^a Princeton University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACETONE; ACTUATORS; BOUNDARY LAYER FLOW; MAGNETIC ACTUATORS; MAGNETOHYDRODYNAMICS; NAVIER STOKES EQUATIONS;

BOUNDARY LAYER INTERACTION; BOUNDARY LAYER SEPARATION CONTROL; BOUNDARY LAYER THICKNESS; COMPUTATIONAL RESULTS; NAVIER-STOKES SOLVER; SCHLIEREN IMAGING; TIME INDEPENDENTS; VOLUMETRIC HEATING;

BOUNDARY LAYERS;

EID: 78049497546     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-1095     Document Type: Conference Paper

References (17)

1. Dolling, David S., Fifty Years of Shock-Wave/Boundary-Layer Interaction Research: What Next? AIAA Journal, Vol. 30, no. 8, pp. 1517-1531, 2001.
2. Lin, J. C., Review of research on low-profile vortex generators to control boundary layer separation Progress in Aerospace Sciences, Vol. 38, pp. 389-420, 2002.
3. Macheret, S.O., Physics of Magnetically Accelerated Nonequilibrium Surface Discharges in High-Speed Flow AIAA-2006-1005, AIAA 44th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 9-12, 2006.
4. Likhanskii, A., Shneider, M., Macheret, S., Miles, R., Modeling of Interaction Between Weakly Ionized Near-Surface Plasmas and Gas Flow AIAA-2006-1204, AIAA 44th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 9-12, 2006.
5. Opiats, D. et. al. Experimental Investigation of DBD Plasma Actuators Driven by Repetitive High Voltage Nanosecond Pulses with DC or Low Frequency Sinusoidal Bias. AIAA-2007-4532, 38th Plasma Dynamics and Lasers Conference, Miami FL, 25-28 June 2007.
6. Kalra C., Zaidi, S., Alderman, B., Miles, R., Non-Thermal Control of Shock-Wave Induced Boundary Layer Separation using Magneto-Hydrodynamics AIAA-2007-4138, 38th Plasma Dynamics and Lasers Conference, Miami FL, 25-28 June 2007.
7. Bogdonoff, S. M., Kepler, E. C., Separation of Supersonic Turbulent Boundary Layer Princeton University, Dept. of Aero. Eng., Report 249, Jan. 1954.
8. Hodge, B. K., Prediction of Hypersonic Laminar Boundary Layer/Shockwave Interactions AIAA Jounal, Vol.15, No 7, pp 903-904, July 1977.
9. Wu M., Bookey P., Martin M. P., Smits A. J., Analysis of shockwave/turbulent boundary layer interaction using DNS and experimental data, AIAA Paper No. 2005-0310, 2005.
10. Kalra, C.S., Zaidi, S., Miles, R., Shockwave Induced Turbulent Boundary Layer Separation Control with Plasma Actuators AIAA Reno, 2008.
11. Anderson J. D., Computational Fluid Dynamics McGraw-Hill Inc., 1995.
12. Shneider M. N., Macheret S.O., Miles R. B., em Electrode Sheaths and Boundary Layers in Hypersonic MHD Channels AIAA Paper 99-3532, 1999.
13. Cebeci T., and Smith A.M.O., Analysis of Turbulent Boundary Layers Academic press, 1974.
14. Schlichting H., Boundary Layer Theory, McGraw-Hill Inc., 1979.
15. Grumet A. A., Anderson J. D., Lewis M. J., A Numerical Study of Shockwave Boundary Layer Interaction in Non-equilibrium Chemically Reacting Air: The effects of Catalytic Walls AIAA-91-0245.
16. Zaidi S., Smith T., Macheret S., Miles R., Snowplow Surface Discharge in Magnetic Field for High Speed Boundary Layer Control AIAA-2006-1006, AIAA 44th Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan. 9-12, 2006.
17. Smith, M. W., Smits, A. J. Visualization of the structure of supersonic turbulent boundary layers. Exp. Fluids 18, 288302, 1995.