Separation Control on HIgh Angle of Attack Airfoil Using Plasma Actuators
作者： Martiqua L. Post , Thomas C. Corke
DOI: 10.2514/1.2929
关键词:
摘要: … One solution to leading-edge separation is to increase the leadingedge radius. This is the … to the boundary layer and prevent flow separation. Although these leading-edge devices are …
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sci-hub.se 参考文章(11)
Thomas C. Corke, Design of Aircraft ,(2002)
C. L. Enloe, Thomas E. McLaughlin, Robert D. VanDyken, K. D. Kachner, Eric J. Jumper, Thomas C. Corke, M. Post, O. Haddad, Mechanisms and Responses of a Dielectric Barrier Plasma Actuator: Geometric Effects AIAA Journal. ,vol. 42, pp. 595- 604 ,(2004) , 10.2514/1.3884
T. C. Corke, D. A. Cavalieri, E. Matlis, Boundary-Layer Instability on Sharp Cone at Mach 3.5 with Controlled Input AIAA Journal. ,vol. 40, pp. 1015- 1018 ,(2002) , 10.2514/2.1744
Gabriel I Font, None, Boundary Layer Control with Atmospheric Plasma Discharges AIAA Journal. ,vol. 44, pp. 1572- 1578 ,(2006) , 10.2514/1.18542
Thomas Corke, Eric Matlis, Phased plasma arrays for unsteady flow control Fluids 2000 Conference and Exhibit. ,(2000) , 10.2514/6.2000-2323
C. L. Enloe, T. E. McLaughlin, G. I. Font, J. W. Baughn, Parameterization of Temporal Structure in the Single Dielectric Barrier Aerodynamic Plasma Actuator AIAA Journal. ,vol. 44, pp. 1127- 1136 ,(2006) , 10.2514/1.16297
Junhui Huang, Thomas C Corke, Flint O Thomas, None, Plasma Actuators for Separation Control of Low-Pressure Turbine Blades AIAA Journal. ,vol. 44, pp. 51- 57 ,(2006) , 10.2514/1.2903
C. L. Enloe, Thomas E. McLaughlin, Robert D. VanDyken, K. D. Kachner, Eric J. Jumper, Thomas C. Corke, Mechanisms and Responses of a Single Dielectric Barrier Plasma Actuator: Plasma Morphology AIAA Journal. ,vol. 42, pp. 589- 594 ,(2004) , 10.2514/1.2305
T. MUELLER, On the historical development of apparatus and techniques for smoke visualization of subsonic and supersonic flows 11th Aerodynamic Testing Conference. ,(1980) , 10.2514/6.1980-420
Thomas Corke, Eric Jumper, Martiqua Post, Dmitriy Orlov, Thomas McLaughlin, APPLICATION OF WEAKLY-IONIZED PLASMAS AS WING FLOW-CONTROL DEVICES 40th AIAA Aerospace Sciences Meeting & Exhibit. ,(2002) , 10.2514/6.2002-350