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❤
I liked the video, I am having a problem studying an assembly where one of the pieces is made of composite material. When placing the assembly in the ACP module, when I go to the setup only the part to which I am going to apply the composite material appears (I understand that it is because I defined it as a surface previously), but when I link the ACP module to the structural static I only see links the composite part and not the entire assembly.
Hi, thanks for the presentation. I was wondering, in the worksheet for defining the layered section it says, "... layers are added to the top, increasing in the +Z normal direction." If this is what you want, then a midsection, layered section is probably not the best application, right? Or you have to redefine your coordinate system?
Thank you, but it doesn't work for me - APDL Post command does not return Tsai Wu failure criterion plot. I got such an error in Post Output: "One or more materials (such as material 2) do not have all required stress or strain strength limits defined. Therefore, no failure criteria are computed" I keyed in material properties for my orthotropic material exactly as you. It seems like APDL cannot read this.
Hi, Mr Pedro Chou, I from Brasil and I would like say thanks for you are sharing your knowledge, i will replicate your lesson. Obrigado !!
Great video! Very good audio quality with clear and helpful guidance
Thank you very much, it really helped me a lot in understanding analysis using ansys
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❤
I liked the video, I am having a problem studying an assembly where one of the pieces is made of composite material. When placing the assembly in the ACP module, when I go to the setup only the part to which I am going to apply the composite material appears (I understand that it is because I defined it as a surface previously), but when I link the ACP module to the structural static I only see links the composite part and not the entire assembly.
Hi, thanks for the presentation. I was wondering, in the worksheet for defining the layered section it says, "... layers are added to the top, increasing in the +Z normal direction." If this is what you want, then a midsection, layered section is probably not the best application, right? Or you have to redefine your coordinate system?
hello,i have a question,what did you do with geometry> sys/solid surface part
sorry, can i ask you a question? how can i see the fiber direction to check my setting is right?
Thank you, but it doesn't work for me - APDL Post command does not return Tsai Wu failure criterion plot. I got such an error in Post Output: "One or more materials (such as material 2) do not have all required stress or strain strength limits defined. Therefore, no failure criteria are computed" I keyed in material properties for my orthotropic material exactly as you. It seems like APDL cannot read this.