期刊文献+

基于Gappy POD的S形扩压器稳态出口流场预测方法研究 被引量:2

Prediction Method Research of Steady Flow Flied for S-shaped Diffuser Based on Gappy POD
下载PDF
导出
摘要 针对实现主动流动控制需要对流场快速获知,提出通过扩压器壁面静压测量值预测出口流场的设想。利用已有的Gappy POD方法实现预测,但该方法在高模态条件下计算精度差。为解决此问题,在已有方法基础上对计算过程中每一步迭代误差进行不同处理,得到Method_1和Method_2。计算结果表明,在静压测点数足够条件下,两种方法能够实现更高精度的计算;并且在不同程度上解决了已有方法在高模态下计算精度差的问题。另外,当测点数达到40时,Method_2计算精度更高。 The idea of using several points of static pressure along the wall to predict the flow flied in the outlet of the S shaped diffuser based on POD is proposed to achieve real time or rapid acquisition of the flow flied. The traditional POD based method is put into use but high accuracy can' t be achieved in high mode number condition. Two different dispose method of iterative err is proposed here to solve that problem. The results show that they can achieve more accurate calculation and lower global err in high mode number if the static pressure measure point is sufficient. additionally,the second method can achieve higher accuracy when the number of measure point reach 40.
出处 《科学技术与工程》 北大核心 2017年第9期84-90,共7页 Science Technology and Engineering
关键词 主动流动控制 S形扩压器 流场预测 改进型Gappy POD active flow control S-shaped diffuser flow flied prediction edited Gappy POD
  • 相关文献

参考文献3

二级参考文献37

  • 1宋立明,李军,丰镇平,罗常.三维跨音速压气机叶栅多目标气动优化设计[J].工程热物理学报,2007,28(2):223-225. 被引量:10
  • 2赵松原,黄明恪.模拟退火算法和POD降阶模态计算在翼型反设计中的应用[J].空气动力学学报,2007,25(2):236-240. 被引量:10
  • 3Abdollah Khodadoust.Active Control of Flow Separation on a High Lift System with Slotted.Flap at High Reynolds Number.AIAA 2007-4424.
  • 4John T Solomon.High Bandwidth Micro-Actuators for Active Flow Control. AIAA 2008-3042.
  • 5Keisuke UDAGAWA. Experimental Study on Supersonic Flow Control by MHD Interaction. AIAA2008-4222.
  • 6Kenneth D. Wright.Measurement Technology for Use in Active Flow Control. AIAA2002--2705.
  • 7NATO.Active Control Technology for Enhanced Performance Operational Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles RTO- MP-051.
  • 8Vikas Kumar.Efficient Control of Separation Using Microjets.AIAA 2005-4879.
  • 9Anthony E. Washburn.Snapshot of Active Flow ControlL Research at NASA Langley.AIAA 2002-3155.
  • 10Scott G. Anders.Active Flow Control Activities at NASA Langley. AIAA-2004-2623.

共引文献50

同被引文献21

引证文献2

二级引证文献4

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部