A transition prediction method for flow over airfoils based on high-order dynamic mode decomposition
turbulence model、experimental data、Stability Theory、novel approach、local Linear、growth rate、new method
32
V11;TG1
the National Natural Science Foundation of China11772261;the Aeronautical Science Foundation of China2016ZA53011;the ATCFD Project2015-F-016;the 111 Project of ChinaNo.B17037.The author would like to thank Prof.Eusebio Valero,Ms.Liu Fangliang,Ms.Han Li and Ms.Wang Shaonan for their guidance and technical support
2019-12-26(万方平台首次上网日期,不代表论文的发表时间)
共14页
2408-2421