Database generated to analyze the effects of a nonadiabatic wall on supersonic shock/boundary-layer interactions

This dataset was generated to analyze the effects of a nonadiabatic wall on supersonic shock/boundary-layer interactions and is related to the following publication: Volpiani, P. S., Bernardini, M., &amp; Larsson, J. (2018). Effects of a nonadiabatic wall on supersonic shock/boundary-layer interactions. <em>Physical Review Fluids</em>, <em>3</em>(8), 083401. The database contains instantaneous and statistical fields of supersonic boundary layers and shock/boundary-layer interactions at free-stream Mach number 2.28. We considered different wall thermal conditions and a wide range of deflection angles. Python scripts are also provided to analyze the data.本数据集专为分析非绝热壁面（nonadiabatic wall）对超音速激波/边界层相互作用（supersonic shock/boundary-layer interactions）的影响而构建，相关联的已发表文献如下：Volpiani, P. S., Bernardini, M., & Larsson, J. (2018). 《非绝热壁面对超音速激波/边界层相互作用的影响》，《物理评论流体（Physical Review Fluids）》，3(8)，083401。该数据库包含来流马赫数（free-stream Mach number）为2.28时，超音速边界层与激波/边界层相互作用的瞬时场与统计场。本研究考虑了多种壁面热边界条件，并覆盖了大范围的偏转角取值范围。同时配套提供了用于数据分析的Python脚本。