Numerical and experimental investigation into hypersonic boundary layer transition induced by roughness elements
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The authors would like to thank the China Scholarship Council;the Aeronautics Science Foundation of China20163252037;the China Postdoctoral Science Foundation2017M610325;the Natural Science Foundation of Jiangsu Province of ChinaBK20170771;the Fundamental Research Funds for the Central Universities of China No.NP2017202 for their support
2019-06-12(万方平台首次上网日期,不代表论文的发表时间)
共9页
559-567