randomwangran/improve

C++GPL-3.0

improve

Using the sequential least squares programming algorit, the drag coefficient for this wing decreases from 0.20031270E-01 to 0.17377422E-01.

What is this?

TODO Using span-wise averaged function to generate runtime data

The goal is to figure out how to use the source code and porting data from v7 to v1906.

The testing code would be in the branch: span-wise-average.

Road map

TODO run with of7/of8 `[0/10]`

TODO find a proper tutorial to play

I find an example, i.e. $FOAM/tutorials/incompressible/simpleFoam/airFoil2D/ very fast to run the test. It's a 2D model.
- TODO issue with airFoil2D
  
  The front and back is defined using the same group.
```
frontAndBack
{
    type empty;
    physicalType empty;
    nFaces 21440;
    startFace 21626;
}
```
  This will make a wrong extrusion.
- TODO test with aerofoilNACA0012
  
  in: $FOAM/tutorials/compressible/rhoSimpleFoam/aerofoilNACA0012
TODO how to extrude 2d mesh?
TODO compile the add-on code
TODO setup the system directory
TODO validate the data is span-wise averaged
TODO try to understand the source code
TODO try to compile it with ofv1906
TODO study the code difference between ofv1906 v.s. of7/of8
TODO translate the of7/8 to ofv1906
TODO test the tutorial case

Contributing

Yes, please do! See CONTRIBUTING for guidelines.

License

See COPYING. Copyright (c) 2020 Ran Wang.