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通过壁面静压测量、流场显示及气动探针测量研究了不同掠型叶片组成的平面扩压叶栅特性.结果表明,前掠叶栅流道中横向压力梯度减弱,型面压力沿叶展呈反"C"型,有利于减弱角区低能流体堆积,但中径处损失有所增加;弯掠叶片强化了上述趋势,其降低端部损失和延缓角区分离的能力更强,应从优化设计角度对其进行深入研究.

参考文献

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[5] 钟兢军.压气机叶栅中应用弯曲叶片的研究[J].航空动力学报,1998(01):7.
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