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In the civil engineering field, most analysis of forces are done on structures. These analyses translate to different kinds of concepts and assumptions.
Here are the general types of structures:
1. Beam – a simple member subjected to transverse loadings and should be properly connected.
P
W
2. Truss – composed of members/
bars assumed to be connected
by frictionless pins; loads are
applied at nodes; members form
triangular divisions.
3. Frames – composed of members
that are connected by rigid joints;
passing a cutting plane through
any point exposes internal shear,
axial and moment at that section.
Trusses are used for two general purposes: (1) as roof trusses and (2) bridge trusses.
For truss analysis, the following assumptions govern:
pin-connected members
Joint/nodal loads only
These assumptions simplify the analysis for the truss. Each truss member may also be called a two-force member because it only resists vertical and horizontal forces, not moments.
A simple truss is a planar truss which begins with a triangular element and can be expanded by adding two members and a joint. For these trusses, the number of members (M) and the number of joints (J) are related by the equation M = 2J -3
Member Forces in trusses maybe characterized into two depending on their direction.
If the member force is towards the joint, the member is under compression.
If the member force is away from the joint, the member is under tension.
Remember that the body we are analyzing is the node or joint.
There are three ways to determine the member forces in trusses, namely:
Method of Joints
Method of Sections
Graphical Method or Maxwell Diagram
Method of Joints
STEPS FOR ANALYSIS
1. If the truss’s support reactions are not given, draw a FBD of
the entire truss and determine the support reactions (typically using scalar equations of equilibrium).
2. Draw the free-body diagram of a joint with one or two
unknowns. Assume that all unknown member forces act in
tension (pulling the pin) or compression (pushing the pin)
3. Apply the scalar equations of equilibrium, Fx = O and
Fy = O, to determine the unknown(s). If the answer is
positive, then the assumed direction is correct,
otherwise it is in the opposite direction.
4. Repeat steps 2 and 3 at each joint in succession until all the
required forces are determined.
If a joint has only two non collinear
members and there is no external load
or support reaction at that joint, then
those two members are zero-force
members. In this example members DE,
DC, AF, and AB are zero force members.
You can easily prove these results by
applying the equations of equilibrium to
joints D and A.
Zero-force members can be removed (as
shown in the figure) when analyzing the
truss.
ZERO-FORCE MEMBERS
If three members form a truss joint for which two of the members are collinear and there is no external load or reaction at that joint, then the third non-collinear member is a zero force member.
* Please note that zero-force members are used to increase stability and rigidity of the truss, and to provide support for various different loading conditions.
ZERO-FORCE MEMBERS
Example 1: Determine the forces in the members of the roof
truss shown in the figure below.
30○
30○ 30○
B
A C
D
100 lb
100 lb
Example 2: The cantilever truss shown in the figure below is
hinged at D and E. Find the force in each member.
A
B
C
D
E
30○ 60○ 60○
10 ft 5 ft
1000 lb
1000 lb 1000 lb
Example 3: Determine the each force member in the figure below
using method of joints
A
B
C D 10ft
10ft
2000lb
30ft
5ft
30○
Example 4: Compute the force in each member of the Warren
truss shown in the figure below.
60○ 60○
B
A C
E
4000 lb
D
60○ 60○
10 ft 10 ft
3000 lb 2000 lb
Example 5: Determine the force in each member of the truss
shown in the figure below using method of joints.
B
A C
300 lb
D
9 ft 9 ft
900 lb 300 lb
E
F
G
12 ft
9 ft H
9 ft 9 ft
9 ft
Example 6: Determine the force in each member of the crane
shown in the figure below using method of joints
A
C
B
E
D
40○
12 ft
4200 lb
9 ft
Example 7: In the cantilever truss shown in the figure below,
compute the force in members AB, BE and DE using method of joints.
(Hint: Use rotation of axis)
A
B
C E H
D
G
30○ 30○
30○
30○
60○
1000 lb
1000 lb
1000 lb
1000 lb
F
Example 8: Determine the member forces using method of joints.
10KN
10KN
10KN
10KN
10KN
1.5m 1.5m 1.5m 1.5m 1.5m 1.5m
1.5m
A
B
C
D
E
F
G
H
I
J
K L
Example 9: The bicycle shown below is loaded with weight =
600N, horizontal load=200N at the seat and 100N at the pedals. Solve for the member forces of the truss
forming the bike.
Assume a hinge
support at A
and roller
at C.
Example 10: Three bars, hinged at A and D and pinned at B and C
as shown, form a four-link mechanism. Determine the value of P that will prevent motion.
P 200 lb
A
B
C
D
75○
45○ 45○
60○
Method of Sections
In the method of sections, a truss is divided into two parts by taking an imaginary “cut” (shown here as a-a) through the truss. Since truss members are subjected to only tensile or compressive forces along their length, the internal forces at the cut members will also be either tensile or compressive with the same magnitude. This result is based on the equilibrium principle and Newton’s third law.
1. Decide how you need to “cut” the truss. This is based on: a) where you need to determine forces, and, b) where the total number of unknowns does not exceed three (in general).
2. Decide which side of the cut truss will be easier to work with (minimize the number of reactions you have to find).
3. If required, determine any necessary support reactions by drawing the FBD of the entire truss and applying the E-of-E.
4. Draw the FBD of the selected part of the cut truss. We need to indicate the unknown forces at the cut members. Initially we may assume all the members are in tension, as we did when using the method of joints. Upon solving, if the answer is positive, the member is in tension as per our assumption. If the answer is negative, the member must be in compression. (Please note that you can also assume forces to be either tension or compression by inspection as was done in the figures above.)
5. Apply the scalar equations of equilibrium (E-of-E) to the
selected cut section of the truss to solve for the unknown
member forces. Please note, in most cases it is possible to write one equation to solve for one unknown directly. So look for it and take advantage of such a shortcut!
Example 11: Determine the force member DG of the Howe truss
shown in the figure below using method of sections.
B
A C
2000 lb
D
12ft 12 ft
1200 lb 800 lb
E
F
G 12 ft 12 ft H
9 ft 9 ft
Example 12: Use the method of sections to determine the forces
in member BD, CD, and CE of the Warren Truss.
60○ 60○
B
A C
E
4000 lb
D
60○ 60○
10 ft 10 ft
3000 lb 2000 lb
Example 13: Determine the force in members AB, BD, BE and
DE of the Howe roof truss shown in the figure below using method of joints and method of
sections.
A
B
C
D
F
H E G
30○ 30○ 30○ 30○
600 lb 1000 lb 400 lb
10 ft 10 ft 10 ft 10 ft
Example 14: The Warren truss loaded as shown in the figure is
supported by a roller at C and a hinge at G. By the method of sections, compute the force in the members BC, DF and CE.
A
20 ft
20 ft
G C
B D
E
20 ft 20 ft
1000 lb 400 lb
600 lb F 800 lb
Example 15: For the truss shown in the figure, determine the force BF
by the method of joints and
then check this result using
method of sections.
(Hint: To apply method
of sections, first
obtain the value
of BE by
inspection.)
12 ft
9 ft
12 ft
9 ft
1200 lb 2400 lb
1200 lb
A
B
C
D
E
F
Example 16: In the fink truss shown in the figure, the web
members BC and EF are perpendicular to the inclined members at their midpoints. Use method of sections to determine the force in members DF, DE and CE.
A
B
C
D
E
F
G
1000 lb 1000 lb
2000 lb
2000 lb
2000 lb
10 ft
40 ft
Example 17: Determine the member forces DF, DG, EG, BD, BE and
CE using method of sections.
10KN
10KN
10KN
10KN
10KN
1.5m 1.5m 1.5m 1.5m 1.5m 1.5m
1.5m
A
B
C
D
E
F
G
H
I
J
K L
Example 18: A beam carrying the loads shown in the figure below is
composed of three segments. It is supported by a four vertical reactions and joined by two frictionless hinges. Determine the values of the reactions.
400 lb 200 lb/ft 100 lb/ft
R1 R2 R3 R4
6 ft 4 ft 4 ft 10 ft 3 ft 3 ft
Hinge Hinge
Example 19: For the frame loaded as shown
in the figure below, determine
the horizontal and vertical
components of the pin
pressure at B. Specify
directions (up or down;
left or right) of the force
as it acts upon members.
A
B
D
C
2ft
4ft
300 lb
200 lb
2ft 2ft
Example 20: A beam carrying the loads shown in the figure below is
composed of three segments. It is supported by a four vertical reactions and joined by two frictionless hinges. Determine the values of the reactions.
100N
300N/m
150N/m
R1 R2 R3 R4
3 m 2 m 2 m 5 m 2 m 2 m
Hinge Hinge
Example 21: A billboard BC weighing
1000lb is subjected to a wind pressure of 300 lb per ft as shown in the figure. Neglecting the weights of the supporting members, determine the components of the hinge forces at A and F.
A
B
C
D
E
F
6 ft 6 ft
4 ft
4 ft
4 ft
2 ft
300
lb
/ft
Example 22: The frame shown in
the figure is supported by a
hinged at E and a roller at
D. Compute the horizontal
and vertical components
of the hinge force at C as
it acts upon BD.
A
E
B
C
D
240 lb
4ft 2ft
8ft
45○ 45○
Example 23: For the frame shown in the figure is supported by a
hinge at A and a roller at E.
Compute the horizontal and
vertical components of the
hinge forces at B and C as they act upon
member AC.
A E
B
C
6ft
4ft
240 lb
2ft 2ft
D
6ft 1ft
Example 24: The bridge shown in the figure consists of two end
sections, each weighing 200 tons with center gravity at G, hinged to a uniform center span weighing 120 tons. Compute the reactions at A,B,E and F.
30 ft 30 ft 20 ft 20 ft 20 ft 20 ft 60 ft
40 ft
40 ft 20 ft 60 tons
G G
A B
C D
E F
Example 25: The frame shown in the figure is hinged at E and
roller supported at A. Determine horizontal and vertical components of the hinge forces at B,C, and D. Neglect the weights of the members
Example 26: Determine the member forces using graphical
method or Maxwell diagram.
10KN
10KN
10KN
10KN
10KN
1.5m 1.5m 1.5m 1.5m 1.5m 1.5m
1.5m
A
B
C
D
E
F
G
H
I
J
K L