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实验研究了不同冲角下子午流道具有较大扩张角的某型低压涡轮导向器原型和改型叶栅的气动性能.结果表明,通过改变端壁型线扩张规律及三维叶型积迭线,改型叶片表面静压分布更加合理,叶栅的流动损失显著减小,流场结构得到明显改善,叶栅气动性能的提高表明改型是成功而且有效的.

参考文献

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