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轴流涡轮基元级动叶稠度特性的数值研究

杨杰 乔渭阳 侯伟涛 魏佐君

杨杰, 乔渭阳, 侯伟涛, 魏佐君. 轴流涡轮基元级动叶稠度特性的数值研究[J]. 航空动力学报, 2012, 27(6): 1288-1296.
引用本文: 杨杰, 乔渭阳, 侯伟涛, 魏佐君. 轴流涡轮基元级动叶稠度特性的数值研究[J]. 航空动力学报, 2012, 27(6): 1288-1296.
YANG Jie, QIAO Wei-yang, HOU Wei-tao, WEI Zuo-jun. Numerical study on the rotor solidity characteristics of axial turbine element stages[J]. Journal of Aerospace Power, 2012, 27(6): 1288-1296.
Citation: YANG Jie, QIAO Wei-yang, HOU Wei-tao, WEI Zuo-jun. Numerical study on the rotor solidity characteristics of axial turbine element stages[J]. Journal of Aerospace Power, 2012, 27(6): 1288-1296.

轴流涡轮基元级动叶稠度特性的数值研究

Numerical study on the rotor solidity characteristics of axial turbine element stages

  • 摘要: 利用商用软件数值模拟了5个不同动叶稠度的轴流涡轮基元级的非定常流动情况,以研究动叶稠度对轴流涡轮基元级性能和流动情况的影响.通过对动叶稠度对基元级反力度、叶片进出口气流角、转子和静子中的流场及损失影响情况的考察研究,发现动叶稠度的改变对涡轮基元性能和流动情况的影响与静叶稠度存在重要关系.静叶稠度不变时,动叶稠度的改变通过影响流过涡轮基元级的流量来使基元级的反力度发生变化.当动叶稠度过大时,气流在转子中会过度膨胀加速而产生激波损失及其与附面层干涉形成的流动分离损失.动叶稠度过小时,转子进口会出现极大的正攻角致使动叶吸力面发生大范围的流动分离.静叶稠度一定时,存在一个最佳的动叶稠度,使涡轮基元级呈现最好的性能.

     

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出版历程
  • 收稿日期:  2011-06-20
  • 刊出日期:  2012-06-28

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