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不同攻角对涡轮叶栅损失的影响

孙大伟 乔渭阳 许开富 李伟

孙大伟, 乔渭阳, 许开富, 李伟. 不同攻角对涡轮叶栅损失的影响[J]. 航空动力学报, 2008, 23(7): 1232-1239.
引用本文: 孙大伟, 乔渭阳, 许开富, 李伟. 不同攻角对涡轮叶栅损失的影响[J]. 航空动力学报, 2008, 23(7): 1232-1239.
SUN Da-wei, QIAO Wei-yang, XU Kai-fu, LI Wei. Influence of different incidences on loss in turbine cascade[J]. Journal of Aerospace Power, 2008, 23(7): 1232-1239.
Citation: SUN Da-wei, QIAO Wei-yang, XU Kai-fu, LI Wei. Influence of different incidences on loss in turbine cascade[J]. Journal of Aerospace Power, 2008, 23(7): 1232-1239.

不同攻角对涡轮叶栅损失的影响

基金项目: 国家自然科学基金(10377011)

Influence of different incidences on loss in turbine cascade

  • 摘要: 应用基于压力修正的三维计算流体动力学(CFD)程序,通过改变进口攻角,对不同工况下的涡轮叶栅流场进行了数值模拟.并结合CFD模拟结果,应用较合理的损失分离方法,对比分析了三种常用的变工况涡轮损失预测模型.结果表明:在正攻角情况下,随着攻角的增加,涡轮叶栅总压损失显著增加;在负攻角情况下,随着攻角的增加,涡轮叶栅总压损失则有种先减小后增大的趋势,但变化范围不大.而对于三种变工况涡轮损失预测模型来说,虽能基本上反映出涡轮损失随攻角的变化趋势,但预测结果差别很大.

     

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出版历程
  • 收稿日期:  2007-07-02
  • 修回日期:  2007-12-20
  • 刊出日期:  2008-07-28

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