




















Study with the several resources on Docsity
Earn points by helping other students or get them with a premium plan
Prepare for your exams
Study with the several resources on Docsity
Earn points to download
Earn points by helping other students or get them with a premium plan
Lecture notes on statically indeterminate structures, focusing on the flexibility and stiffness methods to solve for forces and displacements. The notes cover topics such as equations of equilibrium, compatibility, force-displacement relations, and the use of displacement diagrams. Examples are given to illustrate the concepts.
Typology: Summaries
1 / 28
This page cannot be seen from the preview
Don't miss anything!





















Statically Determinate Structures
can
be determined solely from
free-body diagrams and equations of equilibrium.• Results are
independent
of the material from which the structure
has been made.
10 kN
5 kN
Unknowns = reaction forces + bar forces= (2 + 1) + 13 = 16 Independent equations [equilibrium in x & y directionsat each joint]= 2 (number of joints)= 2 (8) = 16 Double-check structure forinternal mechanisms, etc.
“Flexibility” or “Force” Method
=
A
B
δ
A
δ
A
A
δ
A
Equation of compatibility – expresses the fact that the changein length of the bar must be compatible with the conditions atthe supports
0
2
1
=
=
A
A
A
δ
δ
δ
staticredundant
“released” structure
Write the force-displacement relations. These take the mechanicalproperties of the material into account.
2
1
A
A
A
δ
δ
A
A
A
δ Substituting into the equation of compatibility gives:
A
B
Substituting into the equilibrium equation gives:
*Note that we have solved for forces.Hence, this approach is also called the“force” method. *Note that flexibilities (
b
/
EA
) and (
L
/
EA
)
appear in this equation. Hence, thisapproach is called the “flexibility” method.
Write the force-displacement relations and solve for the forces.
C
B
C
A
B
C
A
C
2
1
2
1
Substituting into the equilibrium equation gives:
C
C
2
1
δ
δ
*Note that stiffnesses (EA/a) and (EA/b)appear in this equation. Hence, thisapproach is called the “stiffness” method.
Using the compatibility condition (displacements equal) gives:
(
)
C
*Note that we have solved for displacement.Hence, this approach is also called the“displacement” method.
Finally, substituting into the expressions for forces gives:
B A
So, both the flexibility method and the stiffness method give thesame result.The choice of approach will depend on the problem being solved.
EquilibriumHorizontal DirectionVertical DirectionMoments about A (ccw +)
4 unknown forces, only 3 equations
R
Ay
T
CD
T
CB
P
R
Ax
L
L α
2
α
1
0
cos
cos
2
1
=
−
−
=
CB
CD
Ax
x
T
T
R
F
0
sin
sin
2
1
=
−
=
P
T
T
R
F
CB
CD
Ay
y
α
α
(
)
(
)
(
)
2
1
CB
CD
A
α
α
CompatibilityWe can relate the tensions in the two wires by considering theextensions of the wires.
δ
D
δ
B
L
L
D
B
δ
δ
2
=
2
1 2
sin
2
sin
sin
D
B
CB
D
CD
=
= =
δ
CD
δ
D
δ
B
δ
CB
Displacement diagram
13
Elasto-plastic Analysis of a Statically Indeterminate Structure
(based on Example 2-19 from Gere)
A
Bar 1
B
P
L
b
b
b
Bar 2
(a)
Find the yield load
P
Y
and the corresponding yield displacement
Δ
BY
at point
B.
(b)
Find the plastic load
P
P
and the corresponding plastic displacement
Δ
BP
at
point B.
(c)
Draw a load-displacement diagram relating the load
P
to the displacement
Δ
B
of point B.
Horizontal beam AB is rigid. Supporting bars 1 and 2 are made of anelastic perfectly plastic material with yield stress
σ
Y
, yield strain
ε
Y
, and
Young’s modulus E =
σ
Y
/
ε
Y
. Each bar has cross-sectional area
A
.
F
1
P
b
b
b
F
2
R
Ax
R
Ay
Moment Equilibrium (ccw +)
(
)
(
)
(
)
2
1
2
1
A
Compatibility
1
2
δ
δ
Force-displacement
2
2
1
1
δ
δ
2 1
Bar 2 will yield first,since
2
1
The corresponding elongation of bar 1 (which has just reachedyield) is:
Y
σ
δ
1
1
1
Note that
P
Y
and
BP
BY
The downward displacement of the bar at point B is:
E
L
Y
BP
3
3
1
=
=
Δ
(b)
B
Y
P
BY
BP
(c)
Bar 2 yields
Bar 1 yields
Bar 2 plastic, bar 1 elastic
Both bars plastic
Bolts and Turnbuckles
Nut and BoltDistance
δ
travelled by the nut =
n p
n
= number of turns (not necessarily an integer)
p
= pitch of the screw (units mm / turn)
Turnbuckle Distance
δ
travelled = 2
n p
Often used to tension cables
Right-hand
screw
Left-hand
screw
The simplest way to produce a change in length.
L
δ
1
δ
1
δ
2
δ
3
P
s
P
s
P
c
The tensile forces in the cables
P
s
and the compressive force in the
tube
P
c
must be such that the final lengths of the cables and tube is the
same.
If the turnbuckles are rotated through
n
turns, the cables will shorten by a
distance
δ
1
= 2
n p
.
Equilibrium (forces must balance)
c
s
Compatibility (shortening of tube must equal shortening of cable)
2
1
3
δ
δ
δ
−
=
Force-displacement
c
c
c
s
s
s
2 3 1
δ δ δ
With these equations, we can solve for the forces in the tube andcables and for the shortening of the tube.