Voilure catia v5

Hello

What is the best method to model the wing of an aircraft under CATIA V5 and how to do it?

Thank you
 

It depends on the final objective of the modeling: flow calculation, manufacturing plan?

What is the input data?

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Re

it's for a finite element calculation (study of the wing)

Thank you

A sweep should be enough if it's for flow.

If it's for structural, you have to make the different pieces...

 

I can't say much more, I don't have CATIA, and I don't fly (at least not outside).

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Hello

A sail is vast. The basis is to make the outer envelope in surface. This way you can use it to limit the structural elements.

After that, you should be more specific about what you want to do.

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Can you give us more info?

on what you want to calculate

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http://www.ipsa.fr/projets-fin-etudes.aspx

Aile de Falcon 2000LX

Study of the shape of a FALCON 2000LX wing

The objective of this project is to study the structural of the FALCON 2000LX wing as well as the aerodynamic characteristics. The 2D modeling under CATIA V5 of the existing wing first made it possible to record the polar and thinness of the wing and to deduce the angle of incidence at which the aircraft stalls.

Subsequently, thanks to 3D modelling, the students recorded the lift forces (between 8000 N and 55000 N) and found the force to be applied to the wing during the structural study. The structural study consisted of several phases.

First, a structural strength study under NASTRAN and then a volume modeling under CATIA made it possible to refine the choices of internal and skin structures. Flow measurements were then made using the FLUENT software for each angle of incidence of the flight envelope.

 

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As the subject is very vast and complex, I took the liberty of putting these links

View this PDF

https://www.google.fr/url?sa=t&rct=j&q=&esrc=s&source=web&cd=2&cad=rja&uact=8&ved=0CCcQFjAB&url=http%3A%2F%2Fflyingmax06.free.fr%2Favion%2Fprojet%2520aero-4a%2Frapport.doc&ei=lX0mVO_KKpDYat3ngLAP&usg=AFQjCNFDMH6AQn3cr908ix0uQwR82eRUbw&sig2=6Cnq_w266iA1tHnBv_03Zg&bvm=bv.76247554,d.d2s

and the google link for this question

https://www.google.fr/webhp?sourceid=chrome-instant&rlz=1C1CHFX_frFR512FR512&ion=1&ie=UTF-8#q=creation+d'une+aile+d'avion+et+etude+structure+sous+catia&spell=1

@+ ;-))

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