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Apply Distributed load to A wing

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 

2 REPLIES
Solution
Solution
Accepted by topic author Mohamed-Ali
‎08-29-2016 02:57 AM

Re: Apply Distributed load to A wing

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

Re: Apply Distributed load to A wing

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 Smiley Happy

 

THANKS