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    姊妹孔平板气膜冷却效率的数值模拟

    Numerical Simulation on Film Cooling Effectiveness with Injection from Sister Holes

    • 摘要: 利用Fluent软件对Navier-Stokes方程进行求解,采用Realizable k-ε 模型研究了30°、45°和60° 3种夹角姊妹孔射流对气膜冷却效率的影响,讨论了2个次孔夹角角度对流动温度场和姊妹孔平板冷却效率的影响.结果表明:姊妹孔主要是通过2个次孔产生的涡旋结构和主孔涡旋结构相互作用来提高冷却效率的,将被抬离的射流中心向横向方向拉拽,破坏反向对涡旋,将升力变为展向拉力,既提高了射流贴壁性又增大了展向覆盖面积;姊妹孔夹角为30°时,平板的气膜冷却效率最高.

       

      Abstract: Using Fluent software to solve the Navier-Stokes equations, the effects of sister hole injection on both the film cooling effectiveness and the surrounding temperature field were studied with Realizable k-ε turbulence models under three angle conditions, namely 30°, 45° and 60°. Results show that the film cooling effectiveness with injection from sister holes is improved by interaction of vortices from two secondary holes and a main hole, which pulls the jet center that has been raised to the crosswise direction, damages the counter-rotating vortex pair, changes the lift force to transverse tensile force, so as to maintain the flow adhesion and improve the transverse distribution of coolant. The highest film cooling effectiveness is to be achieved at an angle of 30° between two sister holes.

       

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