Hi Thomas,

First, I would like to ask you if exist some pythonOCC package for Ubuntu
9.10?

About the (X,Y,Z) arrays structure, I think could be useful the _ThruSection
class along the wing axis! In this case I could combine the algorithm for 2D
geometries (airfoils) to replace the used NACA curves.

By other hand, the arrays from the original algorithm for 3D geometries have
the following structure:

X = (x_point1, x_point2, x_point3, ..., x_pointN)
Y = (y_point1, y_point2, y_point3, ..., y_pointN)
Z = (z_point1, z_point2, z_point3, ..., z_pointN)

I will generate the arrays with real data to be more specific and clear.

Regards!

Marcos.


On 24 April 2010 06:00, <pythonocc-users-requ...@gna.org> wrote:

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>   1. Re: 3D CAD Model from arrays (X, Y,       Z) point        coordinates.
>      (Thomas Paviot)
>
>
> ----------------------------------------------------------------------
>
> Message: 1
> Date: Fri, 23 Apr 2010 13:19:44 +0200
> From: Thomas Paviot <tpav...@gmail.com>
> Subject: Re: [Pythonocc-users] 3D CAD Model from arrays (X, Y,  Z)
>        point   coordinates.
> To: "pythonOCC users mailing list." <pythonocc-users@gna.org>
> Message-ID:
>        <j2qbfc3e86e1004230419z57c44686obd9d1d87dffc7...@mail.gmail.com>
> Content-Type: text/plain; charset="iso-8859-1"
>
> 2010/4/23 Marcos Elgueta Soulat <m.a.elguetasou...@gmail.com>
>
> > Dear pythonOCC-users,
> >
> > I'm working in my final carrer project (Aerospace Engineering), which is
> > related with Parametric Geometry Representation to support Aircraft
> Design
> > Procedures.
> >
> > I implement a mathematic algorithm, able to generate different aircraft
> > components and configurations geometries.
> >
> > I already evaluate this with a simple visualization using MayaVi, but it
> is
> > just a nice picture (Not useful for further analysis). Due to, I would
> like
> > to know:
> >
> > *How can I generate from Python-2.6 a CAD-model in pythonOCC?
> >
> > **Note: the 3D geometry is defined by 3 arrays that contents (X,Y,Z)
> > coordinates respectively?*
> >
> > I appreciate any help!
> >
> > Best Regards,
> >
> > Marcos.
> >
> >
> > --
> > Marcos A. Elgueta Soulat
> > Student of Aerospace Engineering,
> > Department of Mechanics Engineering,
> > University of Concepci?n, Chile.
> >
> > mail: m.a.elguetasou...@gmail.com
> > mobile(1): +56 9 82208407
> > mobile(2): +56 9 83036927
> > skype: marcos.elgueta.soulat
> >
> >
> Hi Marcos,
>
> Welcome to this list.
>
> The difficulty of the surface construction depends on the structure of your
> (x,y,z) arrays. A few months ago, Jelle and I worked on the construction of
> a an aircraft wing surface. It was generated from many NACA curves and the
> use of the _ThruSection class along the wing axis. Could it be of interest
> for your purpose? If the (x,y,z) arrays structure is a triangle or quad
> mesh, it will be much more difficult to generate the BRep surface. Could
> you
> tell us a bit more about your coordinate arrays?
>
> Regards,
>
> Thomas
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-- 
Marcos A. Elgueta Soulat
Student of Aerospace Engineering,
Department of Mechanics Engineering,
University of Concepción, Chile.

mail: m.a.elguetasou...@gmail.com
mobile(1): +56 9 82208407
mobile(2): +56 9 83036927
skype: marcos.elgueta.soulat
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