Mdx top |
Wood Armer bending along panel x axis, top surface |
Mdx bottom |
Wood Armer bending along panel x axis, bottom surface |
Mdy top |
Wood Armer bending along panel y axis, top surface |
Mdy bottom |
Wood Armer bending along panel y axis, bottom surface |
Bearing pressure |
Bearing pressure |
Fx |
Axial force in panel x axis |
Fy |
Axial force in panel y axis |
Fxy |
Complimentary in-plane shear |
Fxz |
Shear in panel z axis in the panel xz plane |
Fyz |
Shear in panel z axis in the panel yz plane |
Mx |
Bending along panel x axis |
My |
Bending along panel y axis |
Mxy |
Plate torsional moment |
σx top |
In-plane axial stress in the x direction, top surface |
σy top |
In-plane axial stress in the y direction, top surface |
τxy top |
In-plane shear stress, top surface |
σx bottom |
In-plane axial stress in the x direction, bottom surface |
σy bottom |
In-plane axial stress in the y direction, bottom surface |
τxy bottom |
In-plane shear stress, bottom surface |
σx max tension |
Maximum tension stress in the x direction for both surfaces = max (σxtop, σxbottom, 0) ≥ 0
|
σy max tension |
Maximum tension stress in the y direction for both surfaces = max (σytop, σybottom, 0) ≥ 0
|
σx max compression |
Maximum compression stress in the x direction for both surfaces = min (σxtop, σxbottom, 0) ≤ 0
|
σy max compression |
Maximum compression stress in the y direction for both surfaces = min (σytop, σybottom, 0) ≤ 0
|
σx in-plane |
In-plane center stress in the x direction |
σy in-plane |
In-plane center stress in the y direction |
σx in-plane tension |
In-plane center tension stress in the x direction = max (σxin-plane, 0) ≥ 0
|
σy in-plane tension |
In-plane center tension stress in the y direction = max (σyin-plane, 0) ≥ 0
|
σx in-plane compression |
In-plane center compression stress in the x direction = min (σxin-plane, 0) ≤ 0
|
σy in-plane compression |
In-plane center compression stress in the y direction = min (σyin-plane, 0) ≤ 0
|