首页> 外文会议>ASME turbo expo: turbomachinery technical conference and exposition >EFFECT OF SOLIDITY ON NON-AXISYMMETRIC ENDWALL CONTOURING PERFORMANCE IN COMPRESSOR LINEAR CASCADES
【24h】

EFFECT OF SOLIDITY ON NON-AXISYMMETRIC ENDWALL CONTOURING PERFORMANCE IN COMPRESSOR LINEAR CASCADES

机译:固含量对压缩机线性梯级非轴对称端壁修整性能的影响

获取原文

摘要

This paper presents both the computational and experimental results to assess the effectiveness of non-axisymmetric endwall contouring in linear cascades under different solidities. Endwalls were designed by geometric scaling of a prior optimized endwall. The results show that the total pressure loss can be reduced by the contoured endwall (CEW) under different solidities. The mechanism of the improvement of CEW is that the adverse pressure gradient (APG) has been reduced mainly through the groove configuration near the leading edge of the suction surface. Besides, the cross-passage pressure gradient (CPG) has also been reduced, which has the benefits to further suppress the corner separation. Moreover, there is an optimum range of the solidity for the CEW. For a lower solidity, the performance of the CEW at +7 degree incidence presents a rapid deterioration, due to the risk of flow separation near the mid-span, for a higher solidity, the profile loss can be more dominant.
机译:本文介绍了计算结果和实验结果,以评估不同密度下线性叶栅中非轴对称端壁轮廓的有效性。通过对先前优化的端壁进行几何缩放来设计端壁。结果表明,在不同密度下,等高线端壁(CEW)可以减少总压力损失。改善CEW的机制是主要通过在吸力表面的前缘附近的凹槽结构来减小反压力梯度(APG)。此外,交叉通道压力梯度(CPG)也被减小,这具有进一步抑制拐角分离的优点。此外,CEW具有最佳的坚固性范围。对于较低的坚固性,由于在中跨附近存在流动分离的风险,因此在+7度入射角下,CEW的性能会迅速变差;对于较高的坚固性,轮廓损失可能会更占优势。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号