Influence of Single Dielectric Barrier Discharge Plasma Actuation on Film Cooling Effect at Plain Surface[J]. 2020, 54(11): 26-36.
DOI:
Influence of Single Dielectric Barrier Discharge Plasma Actuation on Film Cooling Effect at Plain Surface[J]. 2020, 54(11): 26-36.DOI: 10.7652/xjtuxb202011004.
Influence of Single Dielectric Barrier Discharge Plasma Actuation on Film Cooling Effect at Plain Surface
By solving the RANS equations coupled with plasma actuation forces
the influence of single dielectric barrier discharge(SDBD)plasma actuation on film cooling effect at plain surface was numerically investigated. With the experiment data
the reliabilities of linearized plasma force model and numerical methods were validated. Under six different dimensionless actuation strengths
five different dimensionless actuation frequencies and three blowing ratios
the film cooling effects on plain wall surface were predicted. The computed film cooling effectiveness distributions and flow structures near the film cooled surface with SDBD plasma actuation were compared with the cases without plasma actuation. The numerical results show that compared with the case without SDBD actuator
the film cooling effect on plain wall surface is significantly enhanced. With SDBD plasma actuation
the development of counter-rotating kidney vortex pair downstream the cooling hole is suppressed
resulting in a larger near-wall streamwise velocity gradient
higher peak value of near-wall streamwise velocity
and wider coolant coverage along both spanwise and streamwise directions
than the case without plasma actuation. As the dimensionless actuation strength increases from 40 to 140
the film cooling effect on plain wall surface is improved significantly. As the dimensionless actuation strength is equal to 100
the maximum centerline and laterally averaged film cooling effectiveness are increased by 105% and 200% respectively
compared with the case without plasma actuation. As the dimensionless actuation frequency increases from 1.25 to 6.25
the film cooling effectiveness on plain wall surface is kept increasing. When the dimensionless actuation frequency is equal to 3.75
the maximum centerline and laterally averaged film cooling effectiveness on plain wall surface are higher than the case without plasma actuation by 75% and 100% respectively. As the blowing ratio increases
the film cooling effect on plain wall surface is decreased correspondingly. As blowing ratio increases from 0.5 to 1.0
the maximum centerline and laterally averaged film cooling effectiveness on plain wall surface are decreased by 23.9% and 49.2%
respectively.
关键词
Keywords
references
ANDREOPOULOS J, RODI W. Experimental investigation of jets in a cross flow [J]. Journal of Fluid Mechanics, 1984, 138: 93-127.
KOHLI A, BOGARD D G. Adiabatic effectiveness, thermal fields, and velocity fields for film cooling with large angle injection [J]. ASME Journal of Turbomachinery, 1997, 119(2): 352-353.
GOLDSTEIN R J. Film cooling [J]. Advances in Heat Transfer, 1971, 7: 321-379.
LI Heping, YU Daren, SUN Wenting, et al. State-of-the-art of atmospheric discharge plasmas [J]. High Voltage Engineering, 2016, 42(12): 3697-3727.
BAUGHN J W, PORTER C O, PETERSON B L, et al. Momentum transfer for an aerodynamic plasma actuator with an imposed boundary layer [C]∥44th AIAA Aerospace Sciences Meeting and Exhibit. Reston, VA, USA: AIAA, 2006: 168.
COONEY J A, SZLATENYI C S, FINE N E. The development and demonstration of a plasma flow control system on a 20kW wind turbine [C]//54th AIAA Aerospace Sciences Meeting. Reston, VA, USA: AIAA, 2016: 1302.
MARTINEZ D S, PESCINI E, MARRA F, et al. Analysis of the performance of plasma actuators under low-pressure turbine conditions based on experiments and URANS simulations [C]//Proceedings of ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. New York, USA: ASME, 2017: GT2017-64867.
BRIGHT A, TICHENOR N, KREMEYER K, et al. Boundary-layer separation control using laser-induced air breakdown [J]. AIAA Journal, 2018, 56(4): 1472-1482.
COONEY J A, SZLATENYI C S, FINE N E. The development and demonstration of a plasma flow con-trol system on a 20 kW wind turbine [C]∥54th AIAA Aerospace Sciences Meeting. Reston, VA, USA: AIAA, 2016: 1302.
MARTINEZ D S, PESCINI E, MARRA F, et al. Analysis of the performance of plasma actuators under low-pressure turbine conditions based on experiments and URANS simulations [C]∥Proceedings of ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. New York, USA: ASME, 2017: GT2017-64867.
BRIGHT A, TICHENOR N, KREMEYER K, et al. Boundary-layer separation control using laser-induced air breakdown [J]. AIAA Journal, 2018, 56(4): 1472-1482.
AUDIER P, FENOT M, BENARD N, et al. Film cooling effectiveness enhancement using surface dielectric barrier discharge plasma actuator [J]. International Journal of Heat and Fluid Flow, 2016, 62: 247-257.
XUE M, GAO C, XI H D, et al. Vortices induced by a dielectric barrier discharge plasma actuator under burst-mode actuation [J]. AIAA Journal, 2020, 58(6): 2428-2441.
LI G Z, YU J Y, CHEN F, et al. Large eddy simulation of flat plate film cooling flow characteristics based on plasma actuation [C]∥52nd AIAA/SAE/ASEE Joint Propulsion Conference. Reston, VA, USA: AIAA/SAE/ASEE, 2016: 5051.
DE GIORGI M G, TRAFICANTE S, FICARELLA A. Performance improvement of turbomachinery using plasma actuators [C]∥Proceedings of ASME Turbo Expo 2011. New York, USA: ASME, 2011: GT2011 -46413.
SHYY W, JAYARAMAN B, ANDERSSON A. Modeling of glow discharge-induced fluid dynamics [J]. Journal of Applied Physics, 2002, 92(11): 6434-6442.
XUE M, GAO C, XI H D, et al. Vortices induced by a dielectric barrier discharge plasma actuator under burst-mode actuation [J]. AIAA Journal, 2020, 58(6): 2428-2441.
SINHA A K, BOGARD D G, CRAWFORD M E. Film-cooling effectiveness downstream of a single row of holes with variable density ratio [J]. ASME Journal of Turbomachinery, 1991, 113: 442-449.