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Aerodynamic Design Optimization Discussion Group (ADODG)

This page contains the optimized geometry and grid file of the Common Research Model (CRM) wing optimization case for AIAA Aerodynamic Design Optimization Discussion Group (ADODG). Please see the paper 1 for more information.

For a summary of aerodynamic shape optimization in the MDO Lab, see this page.

 

Baseline 28M grid in block-structured CGNS format:

http://mdolab.engin.umich.edu/sites/default/files/Lyu-etal-CRM-baseline-28M.cgns

Baseline 3M grid in block-structured CGNS format:

http://mdolab.engin.umich.edu/sites/default/files/Lyu-etal-CRM-baseline-3M.cgns

Optimized geometry extracted from the 28.8M grid in PLOT3D format:

http://mdolab.engin.umich.edu/sites/default/files/Lyu-etal-CRM-wing-optimized-geometry.xyz

Optimized 28M grid in block-structured CGNS format:

http://mdolab.engin.umich.edu/sites/default/files/Lyu-etal-CRM-optimized-28M.cgns

Optimized 3M grid in block-structured CGNS format:

http://mdolab.engin.umich.edu/sites/default/files/Lyu-etal-CRM-optimized-3M.cgns

Flow conditions:

Reynolds Number: 5.0 million

Mach number: 0.85

 

Movies of the optimization history