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8/13/2019 Seminar05 MPE
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8/13/2019 Seminar05 MPE
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1.1 Example
kinematic boundary conditions: v(0) = 0
v(L) = 0
natural boundary conditions: v (0) = 0
v (L) = 0
1. a11(x) =Z1(x) =A0+A1x+A2x2
kinematic boundary conditions: Z1(0) != 0 A0= 0
Z1(L) != 0 A2= A1
1
L
Z1(x) =A1 x
1
x
L= a11(x) (4)
2. a22(x) =Z2(x) =A3x3 +A4x
4
kinematic boundary conditions: Z2(0) != 0 fulfilled
Z2(L) != 0 A4= A3
1
L
Z2(x) =A3 x3
1
x
L
= a22(x) (5)
3. to n. all other parts analogously
yN(x) =i=1
aii(x) =x
1 x
L
a1+a2x2 +a3x
4 +a4x6 +
(6)
in case of complete series: strict fulfilment of equilibrium conditions(in every point of body = local)
in case of abortion: weak fulfilment of equilibrium conditions(only in weighted integral mean value)
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1.2 Discretization
p(x)
S0
s(x)
x, u
y, v
L
p0
L1
L2
L3
x1
x2
x3I3
I2
I1
discretization e.g. by
mean value
Ii=I(xi= 0) +I(xi= Li)
2
integral mean value
Ii=
Li0
I(xi) dxi
Li
ansatz function for each section
vN(x1) = a0+a1x1+a2x2
1
vN(x2) = b0+b1x2+b2x2
2
vN(x3) = c0+c1x3+c2x2
3
boundary/matching condtions
v(x1= 0) = 0; v(x1= L1) =v(x2= 0) ; v(x2= L2) =v(x3= 0) ;
v (x1= 0) = 0; v (x1= L1) =v
(x2= 0) ; v (x2= L2) =v
(x3= 0) ;
e.g. for L1= L2= L3
vN(x1) = a2x2
vN(x2) = a2
3L
1
3L+ 2x
+b2x
2
vN(x3) = a2
3L (L+ 2x) +
b2
3L+c2x
2
internal potential (without axial strain energy)
i=3
k=1
12
EIk
Lk0
vN(xk)2
dxk
external potential (1st order theory)
ex= 3
k=1
Lk0
p (xk) vN(xk) dx
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2 Minimum potential energy of a plate
x
y
LX
p(x,y) LY
w(x,y)
applied load p (x, y)
displacement field w (x, y)
plate stiffness B= Et3
12(1 2)
potential of internal energy for a plate (derived in lecture)
i= B
2
A
(wxx+wyy)
2 2 (1 )
wxxwyy w
2
xy
dx dy (7)
whereaswxx=
2w
x2, wyy =
2w
y2 and wxy=
2w
xy
potential of external energy
e=
A
p (x, y) w (x, y) dx dy (8)
2.1 Example 1
p (x, y) =p0 sin
xLx
sin
yLy
E, , t, p0= const.
ansatz-function
boundary conditions
w (x= 0, y) = 0 and w (x, y= 0) = 0
w (x= Lx, y) = 0 w (x, y= Ly) = 0
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strong solution (Fourier series)
w (x, y) =a sin
x
Lx
sin
y
Ly
(9)
approximate solution (power series)
wN(x, y) =a
xLx 2 x
3
L3x+ x
4
L4x
yLy 2 y
3
L3y+ y
4
L4y
(10)
strong solution
derivations of displacement function
wx(x, y) = a
Lx cos
x
Lx
sin
y
Ly
wy(
x, y) =
a
Ly
sinx
Lx
cosy
Ly
wxx(x, y) = a
Lx
2 sin
x
Lx
sin
y
Ly
wyy(x, y) = a
Ly
2 sin
x
Lx
sin
y
Ly
wxy(x, y) = a 2
LxLy cos
x
Lx
cos
y
Ly
(11)
internal potential
i = B
2
A
w2xx+ 2wxxwyy+ w
2
yy 2 (1 )
wxxwyy w2
xy
dx dy
= B
2 [I1+ 2I3+I2 2 (1 ) (I3 I4)] (12)
integral I1
I1 =
A
w2xxdx dy = a2
Lx
4
A
sin2
x
Lx
sin2
y
Ly
dx dy
= a2
Lx
4
12
xLx4
sin
2 Lx
x
Lx
0
12
y Ly4
sin
2 Ly
y
Ly
0
= a2
Lx
41
4LxLy (13)
Integral I2
I2=
A
w2yy dx dy = a2
Ly
41
4LxLy (14)
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Integral I3
I3 =
A
wxx wyy dx dy = a2
4
L2xL2y
A
sin2
x
Lx
sin2
y
Ly
dx dy
= a2 4
L2
xL2
y
1
4
LxLy (15)
Integral I4
I4 =
A
w2xydx dy = a2
4
L2xL2y
A
cos2
x
Lx
cos2
y
Ly
dx dy
= a2 4
L2xL2y
1
2x+
Lx
4sin
2
Lxx
Lx
0
1
2y+
Ly
4sin
2
Lyy
Ly
0
= a2 4
L2xL2y
1
4LxLy (16)
finally
i = a2
4
4LxLy
B
2
1
L4x+
2
L2xL2y
+ 1
L4y 2 (1 )
1
L2xL2y
1
L2xL2y
= a24
8LxLyB
1
L2x+
1
L2y
2(17)
external potential
a = A
p (x, y) w (x, y) dx dy = p0aA
sin2
xLx
sin2
yLy
dx dy
= p0a 1
4LxLy (18)
complete potential
=1
4LxLy
a24
B
2
1
L2x+
1
L2y
2p0a
(19)
minimisation principal
a = 0 =
1
4LxLy
2a4
B
2
1
L2x+
1
L2y
2p0
(20)
determination of unknown parameter a
a= p0
B4
1
L2x+ 1
L2y
2 (21)
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2.2 Example 2
ansatz-function
boundary conditions
w (x= 0, y) = 0 and w (x, y= 0) = 0
w (x= Lx, y) = 0 w (x, y= Ly) = 0
w (x= 0, y) = 0
approximate solution (power series)
wN(x, y) =a
x2
L2x
x3
L3x
y
Ly 2
y3
L3y+
y4
L4y
(22)
3 Comparison of strong and approximate solution (Ritz)
structure/system stiffness of approximate solution higher than reality
strong approx
(w) (wN) (23)
displacements of approximate solution lower than reality
w wN (24)
w
n
strong solution
approximatesolution
with displacement w and number of coordinate functions n
7