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

This item contains the following:grids : 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.crm-wb-case-setup-template.txt: setup of Fluent Case filecp : Pressure Coefficient data on the deformed CRM at different angles of attackIf 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.