Can't export points when importing CAD in Blade modelor
(DesignModeler)
Answer:
The problem was with the split in the blade solid. This works when you Boolean/unite the
two solids.
You will also need to ensure the last profile in the Export Points is No
for export, as there is no intersection because of the tip gap. This will export the blade.
1. How is blade tip represented in Turbogrid? the original blade
is flat at tip, Does the blade tip
(Turbogrid) reprensented by the last layer loop cut near the tip? if so, then
the blade geometry has been changed a little at the tip.
2. how to set up the tip shroud gap distance? I noticed the blade
is extends to the shroud in Turbogrid, but the LE (green line in zx
plane/meriondional plane) and TE (red) doesn't not.
3. How is the shape of periodic Boundary ( auxillary view )
defined?
In my mode, the shape of periodic Boundary is highly twisted (not
good for mesing), while the example CAD is good. see attached figures. In
turbogrid tutorial input, I've learned the hub and shourd curves are defined
as curves follow the camber line of blade section (airfoil shape).
Answer:
BladeEditor
generates profiles on surfaces of revolution,
so it will not generate flat profile as you want.
One
option would be use the exiting export points
and write out the crv files.
You will
then need to edit the profile.crv Then add a new profile or replace the last profile with a loop of points for the flat profile.
You can
then load this into TurboGrid and set the Shroud
tip to the last profile. This will cut blade using the specified
profile.
As for the periodic
boundary, it will follow the twist of
the blade. But the generated mesh should give you a reasonable mesh.
Also
note that you can have mesh issues if blade angle is close 90 degree with
regard to axial direction.
Is so
then you will need to use ICEM CFD Hexa to generate a reasonable mesh.
Feedback 2
Typically
wind turbine blades are highly
twisted and as you have noted do not have a shroud. So this cannot be meshed in TurboGrid.
The best option is to use ICEM CFD
Hexa to generate a grid for such blades.
One way to overcome this is to split the blade near the tip, so that you put
an artificial shroud. This can then be
mesh in TurboGrid.
As for the tip section you can generate a mesh
in ICEM CFD Hexa or tetra and use ggi's
to connect the two meshes in CFX
Pre.
Comments
Post a Comment