Hello, thank you very much for this wonderful lecture. I have a question in the ANSYS program. I want to prepare, for example, a superimposed material in the form of a layer consisting of two materials, the first is fiber of any kind, and the other is a polymer material, with dimensions of 10 * 10 cm and a thickness of 2 cm. How do I calculate or how can I enter the volume fraction values For both materials in the ANSYS program, for example, the first material is 60% and the second material is 40%. I hope you will help me in solving this problem. I mean, how can the volumetric fraction or weight ratios be calculated for each materials in the ANSYS program? With appreciation
Hello, thank you very much for this wonderful lecture. I have a question in the ANSYS program. I want to prepare, for example, a superimposed material in the form of a layer consisting of two materials, the first is fiber of any kind, and the other is a polymer material, with dimensions of 10 * 10 cm and a thickness of 2 cm. How do I calculate or how can I enter the volume fraction values For both subjects in the ANSYS program, for example, the first subject is 60% and the second subject is 40%. I hope you will help me in solving this problem. I mean, how can the volumetric fraction or weight ratios be calculated for each subject in the ANSYS program? With appreciation
Thanks Sir for your video. Btw I have a suggestion. Yarn spacing may be the distance between the centers of two yarns. May not be the distance between two yarns.
Good night people,I have a question that I am unable to resolve.After I assemble my woven in material design with carbon woven and epoxy resin I lose the tension and compression properties. How do I resolve this? My analysis will end there in the fault modules, but for that I need all the properties of my woven.Thanks for this video
Thank you for nice explanation. Does E1,E2,E3,G12,G23,G31, NU12,NU13,NU23 are the constants in lamina coordinate (1 2 3) system or in the global coordinate system (x y z)?
Do we have any control over mesh ( like the type of elements ) in Material Designer?
Hello, thank you very much for this wonderful lecture. I have a question in the ANSYS program. I want to prepare, for example, a superimposed material in the form of a layer consisting of two materials, the first is fiber of any kind, and the other is a polymer material, with dimensions of 10 * 10 cm and a thickness of 2 cm. How do I calculate or how can I enter the volume fraction values For both materials in the ANSYS program, for example, the first material is 60% and the second material is 40%. I hope you will help me in solving this problem. I mean, how can the volumetric fraction or weight ratios be calculated for each materials in the ANSYS program? With appreciation
Excellent Video Sir.
Thanks
Hello, thank you very much for this wonderful lecture. I have a question in the ANSYS program. I want to prepare, for example, a superimposed material in the form of a layer consisting of two materials, the first is fiber of any kind, and the other is a polymer material, with dimensions of 10 * 10 cm and a thickness of 2 cm. How do I calculate or how can I enter the volume fraction values For both subjects in the ANSYS program, for example, the first subject is 60% and the second subject is 40%. I hope you will help me in solving this problem. I mean, how can the volumetric fraction or weight ratios be calculated for each subject in the ANSYS program? With appreciation
Thanks Sir for your video. Btw I have a suggestion. Yarn spacing may be the distance between the centers of two yarns. May not be the distance between two yarns.
Good night people,I have a question that I am unable to resolve.After I assemble my woven in material design with carbon woven and epoxy resin I lose the tension and compression properties. How do I resolve this? My analysis will end there in the fault modules, but for that I need all the properties of my woven.Thanks for this video
I am unable to find material designer. how to install it?
same problem, if found solution please tell
@@adityapratapsingh7382 Only on the new version
Only on the new version
Can you do simulation of shaped charge explosion?
Can you do a user defined one please
yes, th-cam.com/channels/UQvPBDppyJ09_3U_fE05sg.html
Results are for ortotropic material?
A question. The final result that appear after “constant material evaluation”.. are values for material homogeneized?
Is this done by ansys workbench2019 ???
Only on the new version
Thank you for nice explanation. Does E1,E2,E3,G12,G23,G31, NU12,NU13,NU23 are the constants in lamina coordinate (1 2 3) system or in the global coordinate system (x y z)?
Lamina coordinate
th-cam.com/channels/UQvPBDppyJ09_3U_fE05sg.html
Thank you, your explanation is very good, it helped me a lot, by the way, are you from India?
th-cam.com/channels/UQvPBDppyJ09_3U_fE05sg.html
Yes, I forgot my id so create a new channel.
@@deepak8057173838 ok