Gao-Yong模型用于吹气环量控制翼型的研究
Study of circulation control airfoil with blowing jet using Gao-Yong turbulence model
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摘要: 应用Gao-Yong湍流模型模拟了吹气对翼型表面分离流控制的影响.结果表明,该模型不仅能够对翼型绕流的分离点、表面压力分布、升阻特性等做出较好预测,而且还能模拟出控制分离的吹气效果:①有效消除翼面分离涡;②"裹携"翼面来流进一步提高升力系数.提高吹气动量系数,升力曲线上移的幅度也相应增加;而吹气角度对吹气射流"裹携"作用的强弱也有一定的影响,当吹气方向相对于翼弦偏上时,吹气射流"裹携"来流与消除分离涡的作用增强,升力提升更为明显.
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关键词:
- 环量控制翼型 /
- Gao-Yong湍流模型 /
- 尾缘吹气 /
- 升力
Abstract: Gao-Yong turbulence model was applied to simulate the influence of blowing jet on the flow separation control of the airfoil surface.The results show that Gao-Yong turbulence model can not only successfully simulate the location of separation and the aerodynamic force coefficients,but also effectively simulate the blowing effect of flow separation control.Other than increasing lift by inhibiting flow separation vortex on the airfoil surface,the blowing jet can also induce much higher lift through the "package effect" for external flow,especially at the condition of large angle of attack.With the increase of blowing jet momentum coefficient,the lift coefficient of the airfoil increases under the same angle of attack.In addition,the angle of the blowing jet has important influence on "package effect".And the positive angle of the blowing jet is more favorable to the lift coefficients than zero and negative angle.-
Key words:
- circulation control airfoil /
- Gao-Yong turbulence model /
- blowing /
- lift
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