DATA: Apetrei et. al. "Using the Reynolds Stress Model to Predict Shock-Induced Separation on Transport Aircraft" Journal Of Aircraft, 56(2), pp. 583–590, 2019
2019-07-17T08:27:09Z (GMT) by
Read the full paper: https://doi.org/10.2514/1.C035027
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 file
cp : Pressure Coefficient data on the deformed CRM at different angles of attack
If any other data is needed that is not available here or in the paper, do not hesitate to contact us and will do our best to make it available.