AIAA-2005-565-450Acoustic Testing of the dielectric barrier(10)
时间:2025-07-09
时间:2025-07-09
推进器的声波特性
References1. List, J., Byerley, A.R., McLaughlin, T.E., and VanDyken, R., “Using Plasma Actuators Flaps to Control Laminar Separation on Turbine Blades in a Linear Cascade”, AIAA 2003-1026, 41st Aerospace Sciences Meeting and Exhibit, 6-9 January 2003, Reno NV. 2. J. Huang, T. Corke, and F. Thomas, “Plasma Actuators for Separation Control of Low Pressure Turbine Blades” 41st Aerospace Sciences Meeting & Exhibit, Reno, NV, 2003, AIAA 2003-1027. 3. Corke, T.C. and Matlis, E., “Phased Plasma Arrays for Unsteady Flow Control”, AIAA 2000-2323, Fluids 2000 Conference, 19-22 June 2000, Denver CO. 4. Post, M.L., and Corke, T.C., “Separation Control of High Angle of Attack Airfoil Using Plasma Actuators”, AIAA 20031024, 41st Aerospace Sciences Meeting and Exhibit, 6-9 January 2003, Reno NV. 5. Corke, T.C., Jumper, E.J., Post, M.L., Orlov, D., and McLaughlin, T.E., “Application of Weakly-Ionized Plasmas as Wing Flow Control Devices”, AIAA 2002-0350, 40th Aerospace Sciences Meeting and Exhibit, 7-10 January 2002. 6. Roth, J.R., Sherman, D.M., Wilkinson, S.P., Boundary Layer Flow Control with a One Atmosphere Uniform Glow Discharge Surface Plasma”, AIAA 98-0328, 36th Aerospace Sciences Meeting and Exhibit, January 12-15, 1998, Reno NV. 7. Roth, J.R., Sherman, D.M., Wilkinson, S.P., “Electrohydrodynamic Flow Control with a Glow-Discharge Surface Plasma”, AIAA J. 38 No. 7, July 2000, p1166-1172. 8. Roth, J.R., Sin, H., Chandra, R., Madhan, M., “Flow Re-Attachment and Acceleration by Paraelectric and Peristaltic Electrohydrodynamic (EHD) Effects”, AIAA 2003-0531, 41st Aerospace Sciences Meeting and Exhibit, 6-9 January 2003, Reno NV. 9. S. Wilkinson, “Investigation of an Oscillating Surface Plasma for Turbulent Drag Reduction,” 41st Aerospace Sciences Meeting & Exhibit, Reno, NV, 2003, AIAA 2003-1023. 10. D. Ashpis and L. Hultgren, “Demonstration of Separation Delay with Glow Discharge Plasma Actuators” 41st Aerospace Sciences Meeting & Exhibit, Reno, NV, 2003, AIAA 2003-1025. 11. Van Dyken, R., McLaughlin, T. E., Enloe, C. L., “Parametric Investigations of a single dielectric barrier plasma actuator”, AIAA 2004-846, 42nd Aerospace Sciences Meeting and Exhibit, 5-8 January 2004, Reno NV. 12. Asghar, A., and Jumper, E.J., “Phase Synchronization of Vortex Shedding from Multiple Cylinders Using Plasma Actuators”, AIAA 2003-1028, 41st Aerospace Sciences Meeting and Exhibit, 6-9 January 2003, Reno NV. 13. Enloe, C.L., McLaughlin, T.E., Van Dyken, R.D., Kachner, K.D., Jumper, E.J., Corke, T.C, “Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology”, AIAA J. 42 No. 3, March 2004, p589-594. 14. Enloe, C.L., McLaughlin, T.E., Van Dyken, R.D., Kachner, K.D., Jumper, E.J., Corke, T.C., Post, M., Haddad, O., “Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Geometric effects”, AIAA J. 42 No. 3, March 2004, p595-604 15. Raichel, Daniel R. The Science and Applications of Acoustics. Springer-Verlag New York, Inc. New York, NY. 2000. 16. Enloe, C.L, McLaughlin T.E, Van Dyken, R.D., Kachner, K.D., Jumper, E.J, Corke, T.C. “Mechanisms and response of a single dielectric barrier plasma”, AIAA 2003-1021, 41st Aerospace Sciences Meeting and Exhibit, 6-9 January 2003, Reno NV.10 American Institute of Aeronautics and Astronautics
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