Your English writing platform
Discover LudwigExact(2)
The obtained results indicate high stress gradients of interlaminar stresses near the edges of laminates.
All results indicate high stress gradients of interlaminar normal and shear stresses near the edges of laminates.
Similar(58)
At the edges of laminate (u_{3}^{left( k right)}) is specified to vanish [see Eq. (35)].
Next, upon substitution of this quantity into the strain displacement relations in (24) and the subsequent results into (8), the interlaminar normal stress σ z is obtained within LWT at the edges of laminate.
It has already been shown that the classical lamination theory is incapable of accurately predicting three-dimensional stress state in region near the edges of laminate known as boundary layer regions.
On the edge of laminates, out-of-plane stresses arise, even up to material's failure.
A new treatment process is developed whereby a layer of resin is applied to the free edges of curved laminates.
Because of substantial importance of boundary layer phenomenon in practical usage enormous research works have been concentrated on the study of interlaminar stresses at free edges of composite laminates.
That is, a thickness away from the edges of the laminate the interlaminar stresses approach zero.
In fact, according to the solution found here, the interlaminar normal stress σ z will vanish at points located on the edges of the laminate at y = ±b.
The following boundary conditions must be imposed at the free edges of the laminate (i.e., at y = ±b): N_{y} = M_{y} = Q_{y} = 0 {text{at}},{text{yy}}, =, pm,{text{b}}.
Write better and faster with AI suggestions while staying true to your unique style.
Since I tried Ludwig back in 2017, I have been constantly using it in both editing and translation. Ever since, I suggest it to my translators at ProSciEditing.

Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com