Instability analysis and drag coefficient prediction on a swept RAE2822 wing with constant lift coefficient

机标关键词：lift coefficient、angle of attack、drag coefficient、civil aircraft、boundary layer、quantitative relationship、pressure coefficient、stability theory、spectral method、mean flow、range of、used in

所属期刊栏目：30

分类号：TV1;O35

资助基金：This study was co-supported by the National Natural Science Foundation of China.11332007,11672351;the Tianjin Natural Science Foundation of China15JCYBJC19500;the Hebei Natural Science Foundation of ChinaA2015105073;an open fund from the State Key Laboratory of Aerodynamics of ChinaSKLA201601

在线出版日期：2017-07-13（万方平台首次上网日期，不代表论文的发表时间）

页数：共12页

页码：964-975