We will now create an alternative geometry 'Tuto6-v2' and check if this updated geometry gives a better result than the first one. This geometry has ducts going from the inlet to the engine cylinders, which may improve their cooling.
Now, we will change a few parameters and parts in the new geometry.
Then import new versions of these parts:
One of the part we replaced had a refinement definition, the part 'Tuto6-v1-1500um.stl. Because this part was removed its refinement definition was automaticaly switched back to the first name available in the list.
Correct the refinement definition by associating it to 'Tuto6-v2-1500um.stl'.
Because we replace two 'reportSurface' parts, the list of flow report surfaces at the bottom of the window also became incorect. Set it back to the correct order : 1 ,2, 3 ; before validating the form with the OK button.
The software will need a couple of minutes to re-process the parts. Then at the bottom of the page showing the geometry parameters, you can hit 'Add a configuration' to define a flight configuration similar to the one created before for the v1:
Go back to the 'Projects' tab and create an analysis similar to the one created before for the geometry v2.