Thank you for the video. Is this theory applicable for laminate subjected to bending loads or Inplane loads . Like irrespective of loading can I use these laminate stack property without giving individual layer properties?
I tried calculating the effective stiffness matrix using the same procedure I developed a code, can you please give some examples so that I can validate
Wonderful Lecture!
fantastic lecture!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!! thank you
Is it valid for filament winding stack?
Nice video professor haha
where can we find lectures 1 and 2
Thank you!!! This is really a Fantanstic Lecture. But How can I get the code?
Hi, would you be able to post the examples you mention at the end? I have written a program to calculate properties and would like to test it.
Hi chris, Did you test your code?
@@vallurusailakshminrusimhap2873 I did and it works beautifully. Thank you for all your help!
Thank you for the video. Is this theory applicable for laminate subjected to bending loads or Inplane loads .
Like irrespective of loading can I use these laminate stack property without giving individual layer properties?
it should work for bending but you should check it
great explanations! could you please also add some books to refer to? thank you very much.
its based on thesis discussed above
I tried calculating the effective stiffness matrix using the same procedure I developed a code, can you please give some examples so that I can validate