DATA for "Using the Reynolds Stress Model to Predict Shock-Induced Separation on Transport Aircraft"

This item contains the following:<br><br><b>grids : </b>ICEM CFD files *.tin and *.blk for the multi-block structured meshes about the NASA CRM deformed at various angles of attack. ICEM CFD is required to rebuild the grids. We are now considering uploading the fully built grids as well.<br><br><b>crm-wb-case-setup-template.txt: </b>setup of Fluent Case file<b><br></b><b>cp : </b>Pressure Coefficient data on the deformed CRM at different angles of attack<br>If any other data is needed that is not available here or in the paper, do not hesitate to contact us and we will do our best to make it available. <br>

本数据集包含以下内容：<br><br><b>网格文件：</b>针对不同攻角下变形的NASA CRM，用于其多块结构化网格的ICEM CFD文件（格式为*.tin与*.blk），需借助ICEM CFD完成该网格的重建工作。目前我们亦在考虑上传已构建完成的完整网格文件。<br><br><b>crm-wb-case-setup-template.txt：</b>Fluent案例文件的配置模板<br><br><b>cp：</b>不同攻角下变形NASA CRM的压力系数（Pressure Coefficient）数据<br>若您需要本数据集或相关论文中未提供的其他数据，请随时与我们联系，我们将尽力为您获取并提供所需内容。