Aug 12, 2004 #1 jimrunner Aerospace Aug 12, 2004 1 I'm looking for formula to determine the Interliminar and shear stress in a composite curved beam. Can anyone help me? Thanks.
I'm looking for formula to determine the Interliminar and shear stress in a composite curved beam. Can anyone help me? Thanks.
Aug 27, 2004 1 #2 happypap Aerospace Aug 18, 2004 6 The interlaminar normal stress in a curved quasi-isotropic laminate can be approximated by -1.5*M/Rm*t where M is the moment per unit length, Rm is the mean radius, and t is the laminate thickness. I think you can find this in the Niu composit book. Upvote 0 Downvote
The interlaminar normal stress in a curved quasi-isotropic laminate can be approximated by -1.5*M/Rm*t where M is the moment per unit length, Rm is the mean radius, and t is the laminate thickness. I think you can find this in the Niu composit book.
