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- Apply Distributed load to A wing

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08-28-2016 04:58 AM

so

if i have a wing and i want to put a load function F(x) = 36.5 - 0.156 *x.^2 which will be change in the dirction of X axis (Parobalci ) in NX 10

How Can I do that.....

i am try but i have this error

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Accepted by topic author Mohamed-Ali

08-29-2016
02:57 AM

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08-28-2016 10:13 AM

M-A,

The problem is that pressure units are force/distance^2 and that the dimension x has units of distance. So you need to make x non-dimensional. You can do this as follows:

36.5 - 0.156-(x/1[mm])^2

Phil

Philippe Tremblay

phillippe.tremblay.ext@siemens.com

www.mayahtt.com

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08-29-2016 02:57 AM

Thank you very much , i am try to write abs(ug_var(x)) and its work , and your answer is another way

thanks for your reply

i have another question if i have the load in N/m not Pa how can i do it

and how can i get friends how work in NX , as a structural analysis

THANKS

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