> On 28 Mar 2019, at 09:24, [email protected] wrote:
> 
> Hi Christophe,
>  
> great picture! How did you create it? When I use the clipping tool it cuts 
> everything.
> How can the clipping be applied to just the surrounding volume?

- Select only "Air" and "Fuselage" in Tools->Visibility, after unchecking 
"recursively"
- Select "Keep whole elements" and "Cut only volume elements" in Tools->Clipping

Christophe

> Many thanks in advance for your answer!
>  
> Best regards,
> Michael
>  
>  
> Von: gmsh <[email protected]> Im Auftrag von Christophe 
> Geuzaine
> Gesendet: Donnerstag, 28. März 2019 08:54
> An: Johannes Dillinger <[email protected]>
> Cc: Gmsh <[email protected]>
> Betreff: Re: [Gmsh] generating an SU2 Euler mesh based on STEP input
>  
> 
> 
> 
> > On 27 Mar 2019, at 22:59, Johannes Dillinger <[email protected]> 
> > wrote:
> > 
> > Hi Christophe,
> > 
> > amazing... thank you for this simplification, really cool!
> > 
> > So the next question would be, if there is an automatic way to specify the 
> > surfaces belonging to the model ("wingfuselage") and the farfield 
> > ("farfield"); I am only able to hard-code it, but there are probably much 
> > smarter ways.. I tried something like
> > Physical Surface("wingfuselage") = Boundary{Volume{v()};};
> > But could not get it to work..
> > 
> > And then I tried to adapt mesh density on the wing and fuselage edges via a 
> > Threshold and Restrict Field. But it seems overly complicated the way I do 
> > it. Do you maybe have a quick suggestion on how to adapt the meshsize in 
> > areas of higher curvature, while leaving it untouched on the farfield?
> > 
> 
> Here's an example:
> 
>  
> 
> <image001.png>
> 
> > I attached again the current status of the .geo-file..
> > 
> > Thanks so much again!
> > Best regards,
> > 
> > Johannes
> > 
> > 
> > 
> > 
> > Am Mi., 27. März 2019 um 19:58 Uhr schrieb Christophe Geuzaine 
> > <[email protected]>:
> > 
> > Hi Johannes,
> > 
> > I can't reproduce the crashes when deleting the curves... Your file also 
> > seems very complicated. I would just do:
> > 
> > SetFactory("OpenCASCADE");
> > Geometry.OCCTargetUnit = "M";
> > v() = ShapeFromFile("wing_fuselage.step");
> > Box(3) = {-5, -5, -5, 10, 10, 10};
> > out() = BooleanDifference{ Volume{3}; Delete; }{ Volume{v()}; Delete; };
> > 
> > out() will contain the volume of interest.
> > 
> > Christophe
> > 
> > 
> >> On 27 Mar 2019, at 19:29, Johannes Dillinger <[email protected]> 
> >> wrote:
> >> 
> >> Dear all,
> >> 
> >> I'm looking for a suitable way to "quickly" generate Euler meshes for SU2 
> >> CFD analysis.
> >> So the usual setup is a (hopefully rather simple) STEP model of a 
> >> wing-fusleage part for example, that I want to mesh in GMSH.
> >> 
> >> I attached a sample STEP and the geo-file that I have been working on, but 
> >> I cant seem to find the errors..
> >>      • First I merge the STEP-file and reverse some surfaces (that 
> >> apparently are oriented in the wrong direction)..
> >>      • I generate a surface loop of the outer surfaces for defining outer 
> >> volume later on. Here the first weird thing happens: the loop command 
> >> generates surfaces 17, 18, and curves 39-44
> >>      • I delete surfaces 17 and 18, since they later on will make problems 
> >> otherwise
> >>      • I also delete the imported volumes
> >> 
> >> I then generate a farfield/bounding box, and also here, the loop command 
> >> generates additional surfaces 1007 to 1010, and I cant figure out why.. 
> >> Anyway, I again delte those, since they will cause problems otherwise.
> >> 
> >> The last problem which really stops me from continuing is the outer volume 
> >> that I generate with the "Volume" command in line 50. This one again 
> >> generates a surface 1009, that I cant delete anymore..
> >> So the surface will be 2D meshed and maybe then leads to the problem that 
> >> the outer volume cannot be meshed.
> >> 
> >> I guess thats enough questions and porblems for now. Once solved, it would 
> >> be great if you could help me with mesh density and so on (already in the 
> >> geo though), but thats for later..:-)
> >> 
> >> So, to sum up:
> >>      • is the general methodology I use ok?
> >>      • how can I avoid the additional surfaces and curves to be created?
> >>      • which problem still exists that does not allow for the 3D mesh 
> >> generation?
> >> Thank you so much in advance!
> >> Best regards,
> >> 
> >> Johannes
> >> 
> >> 
> >> 
> >> 
> >> <wing_fuselage.geo><wing_fuselage.step>_______________________________________________
> >> gmsh mailing list
> >> [email protected]
> >> http://onelab.info/mailman/listinfo/gmsh
> > 
> > — 
> > Prof. Christophe Geuzaine
> > University of Liege, Electrical Engineering and Computer Science 
> > http://www.montefiore.ulg.ac.be/~geuzaine
> > 
> > 
> > 
> > <wing_fuselage.geo>
> 
> — 
> Prof. Christophe Geuzaine
> University of Liege, Electrical Engineering and Computer Science 
> http://www.montefiore.ulg.ac.be/~geuzaine
> 
> 
> 
> _______________________________________________
> gmsh mailing list
> [email protected]
> http://onelab.info/mailman/listinfo/gmsh

— 
Prof. Christophe Geuzaine
University of Liege, Electrical Engineering and Computer Science 
http://www.montefiore.ulg.ac.be/~geuzaine




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