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 Razvan Apetrei Jose Curiel Ning Qin

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.