2. Differential equation of elastic line
Consider a straight beam supported along its
entire length by an elastic medium and
subjected to vertical forces acting in the
principal plane of the symmetrical cross
section.
Let us take infinitely small element enclosed
between two vertical cross-sections at
distance dx apart on the beam under
consideration.
• Assume that this element was taken from a
portion where the beam was acted upon by a
distributed loading q kN/m.
3. The forces exerted on such an element are:
By putting Q = dM/dx,
Using differential equation of a beam in bending, 𝐸𝐼
𝑑2𝑦
𝑑𝑥2 = −𝑀, and
differentiating it twice,
This is the differential equation for the deflection curve of a beam supported on an
elastic foundation.
q
ky
dx
dQ
dx
q
dx
y
k
dQ
Q
Q
0
q
ky
dx
M
d
dx
dQ
2
2
1
......
..........
..........
..........
..........
4
4
2
2
4
4
q
ky
dx
y
d
EI
dx
M
d
dx
y
d
EI
4. Along the unloaded parts of the beam, q = 0, and the equation above will take
the form
It will be sufficient to consider only the general solution of (2),from which
solutions will be obtained by adding to it a particular integral corresponding to q
in (1).
Substituting y = emx in (2), we obtain the characteristic equation:
which has roots:
2
..........
..........
..........
..........
4
4
ky
dx
y
d
EI
EI
k
m
4
i
i
EI
k
m
m
i
i
EI
k
m
m
1
1
4
1
1
4
4
4
2
4
3
1
5. The general solution of (2) takes the form
Where
Using eiλx = cosλx + i sinλx
e-iλx = cosλx - i sinλx
Introducing the new constants C1, C2, C3 and C4, where
We can write
3
...
..........
..........
..........
4
3
2
1
4
3
2
1
x
m
x
m
x
m
x
m
e
A
e
A
e
A
e
A
y
4
4EI
k
4
3
2
3
3
2
2
4
1
1
4
1
;
;
C
A
A
i
C
A
A
C
A
A
i
C
A
A
4
.........
..........
sin
cos
sin
cos 4
3
2
1 x
C
x
C
e
x
C
x
C
e
y x
x
6. The general solution for the deflection line of a straight prismatic bar
supported on an elastic foundation and subjected to transverse bending
forces, but with no surcharge loading (q).
λ is called the characteristic of the system and the inverse is called
characteristic length.
By differentiation of the above equation, we get
x
C
x
C
e
x
C
x
C
e
y x
x
sin
cos
sin
cos 4
3
2
1
x
x
C
x
x
C
e
x
x
C
x
x
C
e
dx
dy
x
x
sin
cos
sin
cos
sin
cos
sin
cos
1
4
3
2
1
7. By differentiation, we get
We know that
x
C
x
C
e
x
C
x
C
e
y x
x
sin
cos
sin
cos 4
3
2
1
x
x
C
x
x
C
e
x
x
C
x
x
C
e
dx
y
d
x
C
x
C
e
x
C
x
C
e
dx
y
d
x
x
C
x
x
C
e
x
x
C
x
x
C
e
dx
dy
x
x
x
x
x
x
sin
cos
sin
cos
sin
cos
sin
cos
2
1
cos
sin
cos
sin
2
1
sin
cos
sin
cos
sin
cos
sin
cos
1
4
3
2
1
3
3
3
4
3
2
1
2
2
2
4
3
2
1
Q
dx
y
d
EI
M
dx
y
d
EI
dx
dy
3
3
2
2
,
,
9. The general solution for the deflection curve of a beam subjected to transverse
loading can be written as:
In this problem, it is reasonable to assume that in an infinite distance from the
application of the load the deflection of the beam must approach zero, that is, if
x→∞, then y→0. Under this condition C1 = C2=0.
Consider a beam of unlimited length in
both directions (an infinite beam)
subjected to a single concentrated force
P at point O.
x
C
x
C
e
x
C
x
C
e
y x
x
sin
cos
sin
cos 4
3
2
1
x
C
x
C
e
y x
sin
cos 4
3
10. From the condition of symmetry, we know that
that is, — (C3 — C4) = 0, from which we find C3 = C4 = C.
This last constant of the equation can be obtained from the consideration
that the sum of the reaction forces will keep equilibrium with the load P,
0
0
x
dx
dy
x
x
Ce
y x
sin
cos
k
P
C
P
kC
P
dx
x
x
e
kC
P
dx
y
k x
2
2
sin
cos
2
2
0
0
11. Substituting the value of C, we have
which gives the deflection curve for the right side (x0) of the beam.
• This deflection curve is a wavy line with decreasing amplitude.
• The deflection under the load is y0 = Pλ/2k.
• The zero points of the line are where cosλx + sinλx = 0, that is, at the
consecutive values of
3
4
𝜋;
7
4
𝜋;
11
4
𝜋 etc.
x
x
e
k
P
y x
sin
cos
2
12. Taking the successive derivatives of y w.r.t. x, we obtain the expressions for θ,
M, and Q on the right side of the beam as
x
e
P
Q
dx
y
d
EI
x
x
e
P
M
dx
y
d
EI
x
e
k
P
dx
dy
x
x
e
k
P
y
x
x
x
x
cos
2
sin
cos
4
sin
sin
cos
2
3
3
2
2
2
15. if (a → 0) Pa will approach the value of M0.
We know the deflection equation for an infinite beam with point load
The above equation can be written as
A concentrated moment M0 is applied M
at point 0 on the infinitely long beam.
This concentrated moment can be
regarded as a limiting case of the loading
shown in Figure.
x
x
e
k
P
y x
sin
cos
2
0
for
2
2
x
a
A
A
k
Pa
A
A
k
P
y x
a
x
x
a
x
16. Since
At the same time
Deflection line due to the M0 clockwise
moment as
x
x
a
x
a
x
B
A
dx
d
a
A
A
2
0
0
0 M
Pa a
x
x
x
x
A
M
Q
dx
y
d
EI
D
M
M
dx
y
d
EI
C
k
M
dx
dy
B
k
M
y
2
2
0
3
3
0
2
2
3
0
2
0
