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i t
(mm)		 xb
(mm)		 yb
(mm)		 xe
(mm)		 ye
(mm)
1 950 0 0 80007000
2 1050 3000 2500 5000 4500
3 - 0 0 00
4 - 0 0 0 0
5 - 0 0 00
i Ks
(kN/m)
1 33000
2 22000
3 -
4 -
5 -
i Vf
(KN)		 Mfx
(kN.m)		 Mfy
(kN.m)		 xL
(mm)		 yL
(mm)
1 -1200 0 0 3000 3500
2 -1200 0 0 5000 3500
i jp xp
(mm)		 yp
(mm)
1 1 1000 1000
2 2 4000 1000
3 1 7000 1000
4 1 1000 6000
5 2 4000 6000
6 1 7000 6000
7 1 1000 3500
8 2 4000 3500
9 1 7000 3500
i t
(mm)		 xb
(mm)		 yb
(mm)		 xe
(mm)		 ye
(mm)
1 950 0 0 80007000
2 1050 3000 2500 5000 4500
3 - 0 0 00
4 - 0 0 0 0
5 - 0 0 00
i Ks
(kN/m)
1 33000
2 22000
3 -
4 -
5 -
i Vf
(KN)		 Mfx
(kN.m)		 Mfy
(kN.m)		 xL
(mm)		 yL
(mm)
1 -1200 0 0 3000 3500
2 -1200 0 0 5000 3500
i jp xp
(mm)		 yp
(mm)
1 1 1000 1000
2 2 4000 1000
3 1 7000 1000
4 1 1000 6000
5 2 4000 6000
6 1 7000 6000
7 1 1000 3500
8 2 4000 3500
9 1 7000 3500
i Ks
(kN/m)
1 33000
2 22000
3 -
4 -
5 -
i t
(mm)		 xb
(mm)		 yb
(mm)		 xe
(mm)		 ye
(mm)
1 950 0 0 80007000
2 1050 3000 2500 5000 4500
3 - 0 0 00
4 - 0 0 0 0
5 - 0 0 00
i Vf
(KN)		 Mfx
(kN.m)		 Mfy
(kN.m)		 xL
(mm)		 yL
(mm)
1 -1200 0 0 3000 3500
2 -1200 0 0 5000 3500
i jp xp
(mm)		 yp
(mm)
1 1 1000 1000
2 2 4000 1000
3 1 7000 1000
4 1 1000 6000
5 2 4000 6000
6 1 7000 6000
7 1 1000 3500
8 2 4000 3500
9 1 7000 3500
Pile-Mat Foundation (FEA)
mm Lx = General Information E0 = Ly = mm MPa m = q0 = kPa
Notes: Plate is analysed by Finite Element Method (Bilinear Mindlin Bending Plate Element) M x = moment per unit width, stretching the fibers in X - direction M y = moment per unit width, stretching the fibers in Y - direction M xy = twisting moment may be used to add to the effect of orthogonal moments Mx and My for the purpose of determing the steel reinforcement Q y = shear per unit width, on the plane perpendicular to axis Y Q x = shear per unit width, on the plane perpendicular to axis X Units: Shear- kN/m; moment - kN.m/m; deflection - mm Instruction: The origin of coordinate system is at the lower left corner For uniform loading (q 0) and vertical loading (V f), out of screen (tension) is positive, otherwise, it is negative For flexural moment about Y axis, streching the fibers in X direction (M fx), with right hand rule, positive in Y dirction For flexural moment about X axis, streching the fibers in Y direction (M fy), with right hand rule, positive in X dirction Considering layout of plate thickness, and locations of piles and loading, this function meshes the whole plate to elements automatically and intelligently If adjacent loading or piles are less than element size /4, please combine the loading or piles in one location Input the loading for one location in one load case If there is crossing rectangular area of two types of plate thickness, the latest thickness layout will cover the previous one Select Add, Click button Edit will add item i to the table Select Delete , Click button Edit will delete item i from the table Select Update, Click button Edit will change item i of the table You couldn't Add or Delete item 1, but you can Update item 1 Reference: Concepts and Applications of Finite Element Analysis, 3rd Edition, Cook, R. D., John Wiley & Sons
jp = i = xp = yp = mm mm Pile Locations
Vf = kN i = xL = yL = mm mm Loading kN.m Mfx = Mfy = kN.m
ks = kN/m i = Pile Types
t = mm i = xe = ye = mm mm Plate Thickness mm xb = yb = mm
Mxmin = kN.m/m kN.m/m Maximum Internal Forces Mxmax = Mymin = kN.m/m kN.m/m kN/m Dmax = mm Mymax = kN/m kN/m kN/m Qymin = Qxmin = Qymax = Qxmax =
Pile-Mat Foundation (FEA)Review Report