chikko04
Guest
Hi, guys, I'm still here asking for help with Patran. I'm a student, so I'm still learning and that such software makes us use it to the segregated member without explaining.
the new exercise is the study of the buckilng phenomenon on a square plate of sizes 1x1 m and thickness 0.001m of aluminum, rested and hinged on the 4 sides loaded on one of them with a distributed load so that the total is 1n.
Now putting these 3d constraints is one of my first problems.
I get to impose then:
for long sides x: t2=0,t3=0,r2=0,r3=0
for long sides y: t1=0,t3=0,r1=0,r3=0
in advance that my problem comes from the fact that I have 3 sizes.
the mesh is a 10x10
for the load I use the function "distribuited load" but I did not even find online if (as I suppose) the value to be inserted is the total load or I must insert the fractional load according to the nodes.
After that (having set as isotropic and aluminum property and as a shell structure) I choose the solutor 105.
at this point, as from the theory and videos on you tube I expect of the "modes" of vibration as output, while instead I receive only a static analysis, which returns me deformation nothing (of course add seen the constraints).
Now someone can tell me, if and where am I wrong and why?
Thank you for your patience.
the new exercise is the study of the buckilng phenomenon on a square plate of sizes 1x1 m and thickness 0.001m of aluminum, rested and hinged on the 4 sides loaded on one of them with a distributed load so that the total is 1n.
Now putting these 3d constraints is one of my first problems.
I get to impose then:
for long sides x: t2=0,t3=0,r2=0,r3=0
for long sides y: t1=0,t3=0,r1=0,r3=0
in advance that my problem comes from the fact that I have 3 sizes.
the mesh is a 10x10
for the load I use the function "distribuited load" but I did not even find online if (as I suppose) the value to be inserted is the total load or I must insert the fractional load according to the nodes.
After that (having set as isotropic and aluminum property and as a shell structure) I choose the solutor 105.
at this point, as from the theory and videos on you tube I expect of the "modes" of vibration as output, while instead I receive only a static analysis, which returns me deformation nothing (of course add seen the constraints).
Now someone can tell me, if and where am I wrong and why?
Thank you for your patience.