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

dataset
posted on 08.04.2021, 16:38 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 we will do our best to make it available.

Funding

The University of Sheffield

History

Ethics

There is no personal data or any that requires ethical approval

Policy

The data complies with the institution and funders' policies on access and sharing

Sharing and access restrictions

The data can be shared openly

Data description

  • The file formats are open or commonly used

Methodology, headings and units

  • There is a readme.txt file describing the methodology, headings and units

Licence

Exports

Department of Mechanical Engineering

Licence

Exports