RPstress
Aerospace
- Jun 4, 2003
- 846
I have a note I made some time ago which says that for a plate with significant shear-extension coupling (A13<>0), the modulus will vary with the length-to-width ratio. I even have an equation for it. If Ex is the theoretical classical plate modulus (i.e., for an infinite plate) then the modulus Ex' of a finite strip would be:
Ex' = Ex * [ 1 - 3*A13^2/(3*A11*A33 + 2*A11^2*L/W) ]
However, like a fool I didn't note the reference when I made the note, and I can't find it mentioned anywhere in my current refs. Does anybody know if there's any truth in this statement and equation??
-R.
Ex' = Ex * [ 1 - 3*A13^2/(3*A11*A33 + 2*A11^2*L/W) ]
However, like a fool I didn't note the reference when I made the note, and I can't find it mentioned anywhere in my current refs. Does anybody know if there's any truth in this statement and equation??
-R.