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Effect of solidity on non-axisymmetric endwall contouring performance in compressor linear cascades

  • Beihang University
  • Collaborative Innovation Center for Advanced Aero-Engine

科研成果: 书/报告/会议事项章节会议稿件同行评审

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.

源语言英语
主期刊名Turbomachinery
出版商American Society of Mechanical Engineers (ASME)
ISBN(印刷版)9780791850992
DOI
出版状态已出版 - 2018
活动ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition, GT 2018 - Oslo, 挪威
期限: 11 6月 201815 6月 2018

出版系列

姓名Proceedings of the ASME Turbo Expo
2A-2018

会议

会议ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition, GT 2018
国家/地区挪威
Oslo
时期11/06/1815/06/18

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