首页> 外文期刊>Aerospace science and technology >Control mechanisms of endwall profiling and its comparison with bowed blading on flow field and performance of a highly-loaded compressor cascade
【24h】

Control mechanisms of endwall profiling and its comparison with bowed blading on flow field and performance of a highly-loaded compressor cascade

机译:端壁轮廓控制机理及其与弓形叶片流场和高负荷压缩机叶栅性能的比较

获取原文
获取原文并翻译 | 示例
       

摘要

In order to exploit the control mechanism of endwall profiling (EP) on flow field and performance of compressors, this paper carried out investigations on non-axisymmetric endwall profiling (NAEP), axisymmetric endwall profiling (AEP) and the comparison with bowed blading in a highly-loaded compressor cascade. Firstly, the influence mechanism of NAEP on corner separation and its design strategies were investigated. Pattern effect of NAEP, axial effect and height effect of concave/convex of NAEP were studied. Secondly, the influence mechanism of AEP on corner separation and its design strategies were studied. Thirdly, the comparison of flow mechanism between endwall profiling (EP) and bowed blading was carried out. Results show that although all the NAEP patterns can reduce the cross-passage pressure gradient, they exhibit distinct different control effects on corner separation. It is indicated that the radially inward pressure gradient, rather than the cross-passage pressure gradient near the endwall, is the key to control corner separations. The endwall cross-passage pressure gradient remained after AEP. However, the corner separation was also eliminated effectively by AEP with a concave curvature, with loss coefficient reduced by 20.07%. At last, compared with bowed blading, the cascade with EPs exhibits a higher overall performance but a lower control effect on corner separation. (C) 2019 Elsevier Masson SAS. All rights reserved.
机译:为了探索端壁轮廓图(EP)对压缩机流场和性能的控制机制,本文对非轴对称端壁轮廓图(NAEP),轴对称端壁轮廓图(AEP)进行了研究,并与弓形叶片进行了比较。高负荷的压缩机级联。首先,研究了NAEP对拐角分离的影响机理及其设计策略。研究了NAEP的图案效应,NAEP凹凸的轴向效应和高度效应。其次,研究了AEP对拐角分离的影响机理及其设计策略。第三,比较了端壁轮廓(EP)和弓形叶片之间的流动机理。结果表明,尽管所有的NAEP模式都可以减小交叉通道压力梯度,但是它们对拐角分离表现出截然不同的控制效果。结果表明,径向向内的压力梯度而不是端壁附近的交叉通道压力梯度是控制拐角分离的关键。 AEP后仍保留端壁交叉通道压力梯度。但是,具有凹曲率的AEP还可以有效地消除拐角分离,损耗系数降低了20.07%。最后,与弓形叶片相比,带有EP的叶栅具有较高的整体性能,但对角部分离的控制效果较低。 (C)2019 Elsevier Masson SAS。版权所有。

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