机译:雷诺数很低的介质阻挡放电流量控制
AR: aspect ratio; C_D: semispan drag coefficient; C_d: airfoil drag coefficient; C_L: semispan lift coefficient; C_t: airfoil lift coefficient; C_P: power coefficient; Cμ: mean momentum coefficient, J/q∞c; c_μ: oscillatory momentum coefficient, J/q_∞c; c: model chord length; DC: duty cycle; F~+: reduced excitation frequency, f_mX_(te)/U_∞; f_c: plasma carrier frequency; f_m: modulation or pulsation frequency, 1/T_m; J: time-mean actuator momentum; J: oscillatory actuator momentum; m: mass; P: power; q_∞: freestream dynamic pressure; Re: Reynolds number based on chord length; s: wing semispan length, b/2; T_m: burst period, 1/f_m; t: time; U_∞: freestream velocity; U,V,W: mean velocity components; u,v,w: instantaneous jet velocity components; X_(te): distance from the actuator upper;
机译:低雷诺数的介质阻挡放电等离子体致动器进行层流分离流控制的机制
机译:使用介质阻挡放电致动器的低雷诺数空气动力学自适应流量控制
机译:通过微秒脉冲介质屏障排放在高雷诺数的飞行翼流分离控制
机译:极低飞行雷诺数的介质屏障排放流量控制
机译:使用介电势垒放电执行器的低雷诺数自适应流量控制。
机译:用于主动流量控制的微型单介质阻挡放电等离子体致动器的耗散功率和感应速度场数据
机译:利用介质屏障放电致动器的低雷诺数空气动力学的自适应流量控制