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Moses失速模型三维优化修正

张兴发 李军 宋国兴

张兴发, 李军, 宋国兴. Moses失速模型三维优化修正[J]. 航空动力学报, 2019, 34(12): 2719-2728. doi: 10.13224/j.cnki.jasp.2019.12.021
引用本文: 张兴发, 李军, 宋国兴. Moses失速模型三维优化修正[J]. 航空动力学报, 2019, 34(12): 2719-2728. doi: 10.13224/j.cnki.jasp.2019.12.021
ZHANG Xingfa, LI Jun, SONG Guoxing. Three-dimensional optimization correction of Moses stall model[J]. Journal of Aerospace Power, 2019, 34(12): 2719-2728. doi: 10.13224/j.cnki.jasp.2019.12.021
Citation: ZHANG Xingfa, LI Jun, SONG Guoxing. Three-dimensional optimization correction of Moses stall model[J]. Journal of Aerospace Power, 2019, 34(12): 2719-2728. doi: 10.13224/j.cnki.jasp.2019.12.021

Moses失速模型三维优化修正

doi: 10.13224/j.cnki.jasp.2019.12.021
基金项目: 国家自然科学基金(51336011)

Three-dimensional optimization correction of Moses stall model

  • 摘要: 通过低速轴流压气机失速实验,结合压气机失速仿真云图以及实验中所测得的叶片径向压力脉动图,发现失速后为部分叶高失速,而不是全叶高失速。基于失速预测Moses模型,通过比较不同径向截面计算得到的总压损失,发现沿径向叶片截面安装角的变化对模型的计算结果有影响,通过引入参数B对模型中的参数k进行改进。经过改进后的模型所预测的结果较原模型能够更加准确地预测压气机失速后的情况,改进后的模型可以为压气机设计提供良好的参考设计数据。对高亚声速轴流压气机进行改进,将高速可压这一因素考虑到模型推导中,对模型进行改进,改进后的模型相较于原模型在预测计算高亚声速轴流压气机压比特性上准确度提升了30%。

     

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出版历程
  • 收稿日期:  2019-07-15
  • 刊出日期:  2019-12-28

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