Kiến trúc xây dựng - Mechanics of materials
          
        
            
            
              
            
 
            
                
                    SOLUTION:
• Taking the entire beam as a free body,
determine the reactions at A and D.
• Apply the relationship between shear and
load to develop the shear diagram.
Draw the shear and bending
moment diagrams for the beam
and loading shown.
• Apply the relationship between bending
moment and shear to develop the bending
moment diagram
                
              
                                            
                                
            
 
            
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MECHANICS OF 
MATERIALS
Third Edition
Ferdinand P. Beer
E. Russell Johnston, Jr.
John T. DeWolf
Lecture Notes:
J. Walt Oler
Texas Tech University
CHAPTER
© 2002 The McGraw-Hill Companies, Inc. All rights reserved.
Analysis and Design
of Beams for Bending
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 2
Analysis and Design of Beams for Bending
Introduction
Shear and Bending Moment Diagrams
Sample Problem 5.1
Sample Problem 5.2
Relations Among Load, Shear, and Bending Moment
Sample Problem 5.3
Sample Problem 5.5
Design of Prismatic Beams for Bending
Sample Problem 5.8
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 3
Introduction
• Beams - structural members supporting loads at 
various points along the member
• Objective - Analysis and design of beams
• Transverse loadings of beams are classified as 
concentrated loads or distributed loads
• Applied loads result in internal forces consisting 
of a shear force (from the shear stress 
distribution) and a bending couple (from the 
normal stress distribution)
• Normal stress is often the critical design criteria
S
M
I
cM
I
My
mx ==−= σσ
Requires determination of the location and 
magnitude of largest bending moment
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 4
Introduction
Classification of Beam Supports
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 5
Shear and Bending Moment Diagrams
• Determination of maximum normal and 
shearing stresses requires identification of 
maximum internal shear force and bending 
couple.
• Shear force and bending couple at a point are 
determined by passing a section through the 
beam and applying an equilibrium analysis on 
the beam portions on either side of the 
section.
• Sign conventions for shear forces V and V’
and bending couples M and M’
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 6
Sample Problem 5.1
For the timber beam and loading 
shown, draw the shear and bend-
moment diagrams and determine the 
maximum normal stress due to 
bending.
SOLUTION:
• Treating the entire beam as a rigid 
body, determine the reaction forces
• Identify the maximum shear and 
bending-moment from plots of their 
distributions.
• Section the beam at points near 
supports and load application points. 
Apply equilibrium analyses on 
resulting free-bodies to determine 
internal shear forces and bending 
couples
• Apply the elastic flexure formulas to 
determine the corresponding 
maximum normal stress.
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 7
Sample Problem 5.1
SOLUTION:
• Treating the entire beam as a rigid body, determine 
the reaction forces
∑ ∑ ==== kN14kN40:0 from DBBy RRMF
• Section the beam and apply equilibrium analyses 
on resulting free-bodies
( )( ) 00m0kN200
kN200kN200
111
11
==+∑ =
−==−−∑ =
MMM
VVFy
( )( ) mkN500m5.2kN200
kN200kN200
222
22
⋅−==+∑ =
−==−−∑ =
MMM
VVFy
0kN14
mkN28kN14
mkN28kN26
mkN50kN26
66
55
44
33
=−=
⋅+=−=
⋅+=+=
⋅−=+=
MV
MV
MV
MV
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 8
Sample Problem 5.1
• Identify the maximum shear and bending-
moment from plots of their distributions.
mkN50kN26 ⋅=== Bmm MMV
• Apply the elastic flexure formulas to 
determine the corresponding 
maximum normal stress.
( )( )
36
3
36
2
6
12
6
1
m1033.833
mN1050
m1033.833
m250.0m080.0
−
−
×
⋅×==
×=
==
S
M
hbS
B
mσ
Pa100.60 6×=mσ
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 9
Sample Problem 5.2
The structure shown is constructed of a 
W10x112 rolled-steel beam. (a) Draw 
the shear and bending-moment diagrams 
for the beam and the given loading. (b) 
determine normal stress in sections just 
to the right and left of point D.
SOLUTION:
• Replace the 10 kip load with an 
equivalent force-couple system at D. 
Find the reactions at B by considering 
the beam as a rigid body.
• Section the beam at points near the 
support and load application points. 
Apply equilibrium analyses on 
resulting free-bodies to determine 
internal shear forces and bending 
couples.
• Apply the elastic flexure formulas to 
determine the maximum normal 
stress to the left and right of point D.
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 10
Sample Problem 5.2
SOLUTION:
• Replace the 10 kip load with equivalent force-
couple system at D. Find reactions at B.
• Section the beam and apply equilibrium 
analyses on resulting free-bodies.
( )( ) ftkip5.1030 kips3030
:
2
2
1
1 ⋅−==+∑ =
−==−−∑ =
xMMxxM
xVVxF
CtoAFrom
y
( ) ( ) ftkip249604240
kips240240
:
2 ⋅−==+−∑ =
−==−−∑ =
xMMxM
VVF
DtoCFrom
y
( ) ftkip34226kips34
:
⋅−=−= xMV
BtoDFrom
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 11
Sample Problem 5.2
• Apply the elastic flexure formulas to 
determine the maximum normal stress to 
the left and right of point D.
From Appendix C for a W10x112 rolled 
steel shape, S = 126 in3 about the X-X axis.
3
3
in126
inkip1776
:
in126
inkip2016
:
⋅==
⋅==
S
M
DofrighttheTo
S
M
DoflefttheTo
m
m
σ
σ ksi0.16=mσ
ksi1.14=mσ
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 12
Relations Among Load, Shear, and Bending Moment
( )
xwV
xwVVVFy
∆−=∆
=∆−∆+−=∑ 0:0
∫−=−
−=
D
C
x
x
CD dxwVV
w
dx
dV
• Relationship between load and shear:
( )
( )221
0
2
:0
xwxVM
xxwxVMMMMC
∆−∆=∆
=∆∆+∆−−∆+=∑ ′
∫=−
=
D
C
x
x
CD dxVMM
dx
dM 0
• Relationship between shear and bending 
moment:
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 13
Sample Problem 5.3
SOLUTION:
• Taking the entire beam as a free body, 
determine the reactions at A and D.
• Apply the relationship between shear and 
load to develop the shear diagram.
Draw the shear and bending 
moment diagrams for the beam 
and loading shown.
• Apply the relationship between bending 
moment and shear to develop the bending 
moment diagram.
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 14
Sample Problem 5.3
SOLUTION:
• Taking the entire beam as a free body, determine the 
reactions at A and D.
( ) ( )( ) ( )( ) ( )( )
kips18
kips12kips26kips12kips200
0F
kips26
ft28kips12ft14kips12ft6kips20ft240
0
y
=
−+−−=
=∑
=
−−−=
=∑
y
y
A
A
A
D
D
M
• Apply the relationship between shear and load to 
develop the shear diagram.
dxwdVw
dx
dV −=−=
- zero slope between concentrated loads
- linear variation over uniform load segment
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 15
Sample Problem 5.3
• Apply the relationship between bending 
moment and shear to develop the bending 
moment diagram.
dxVdMV
dx
dM ==
- bending moment at A and E is zero
- total of all bending moment changes across 
the beam should be zero
- net change in bending moment is equal to 
areas under shear distribution segments
- bending moment variation between D 
and E is quadratic
- bending moment variation between A, B, 
C and D is linear
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 16
Sample Problem 5.5
SOLUTION:
• Taking the entire beam as a free body, 
determine the reactions at C.
• Apply the relationship between shear 
and load to develop the shear diagram.
Draw the shear and bending moment 
diagrams for the beam and loading 
shown.
• Apply the relationship between 
bending moment and shear to develop 
the bending moment diagram.
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 17
Sample Problem 5.5
SOLUTION:
• Taking the entire beam as a free body, 
determine the reactions at C.
⎟⎠
⎞⎜⎝
⎛ −−=+⎟⎠
⎞⎜⎝
⎛ −==∑
=+−==∑
33
0
0
02
1
02
1
02
1
02
1
aLawMMaLawM
awRRawF
CCC
CCy
Results from integration of the load and shear 
distributions should be equivalent.
• Apply the relationship between shear and load 
to develop the shear diagram.
( )curveloadunderareaawV
a
xxwdx
a
xwVV
B
a
a
AB
−=−=
⎥⎥⎦
⎤
⎢⎢⎣
⎡
⎟⎟⎠
⎞
⎜⎜⎝
⎛ −−=∫ ⎟⎠
⎞⎜⎝
⎛ −−=−
02
1
0
2
0
0
0 2
1
- No change in shear between B and C.
- Compatible with free body analysis
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 18
Sample Problem 5.5
• Apply the relationship between bending moment 
and shear to develop the bending moment 
diagram.
2
03
1
0
32
0
0
2
0 622
awM
a
xxwdx
a
xxwMM
B
a
a
AB
−=
⎥⎥⎦
⎤
⎢⎢⎣
⎡
⎟⎟⎠
⎞
⎜⎜⎝
⎛ −−=∫ ⎟⎟⎠
⎞
⎜⎜⎝
⎛
⎟⎟⎠
⎞
⎜⎜⎝
⎛ −−=−
( ) ( )
( ) ⎟⎠
⎞⎜⎝
⎛ −=−−=
−−=∫ −=−
32
3 006
1
02
1
02
1
aLwaaLawM
aLawdxawMM
C
L
a
CB
Results at C are compatible with free-body 
analysis
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 19
Design of Prismatic Beams for Bending
• The largest normal stress is found at the surface where the 
maximum bending moment occurs.
S
M
I
cM
m
maxmax ==σ
• A safe design requires that the maximum normal stress be 
less than the allowable stress for the material used. This 
criteria leads to the determination of the minimum 
acceptable section modulus.
all
allm
M
S σ
σσ
max
min =
≤
• Among beam section choices which have an acceptable 
section modulus, the one with the smallest weight per unit 
length or cross sectional area will be the least expensive 
and the best choice.
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 20
Sample Problem 5.8
A simply supported steel beam is to 
carry the distributed and concentrated 
loads shown. Knowing that the 
allowable normal stress for the grade 
of steel to be used is 160 MPa, select 
the wide-flange shape that should be 
used.
SOLUTION:
• Considering the entire beam as a free-
body, determine the reactions at A and 
D.
• Develop the shear diagram for the 
beam and load distribution. From the 
diagram, determine the maximum 
bending moment.
• Determine the minimum acceptable 
beam section modulus. Choose the 
best standard section which meets this 
criteria.
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 21
Sample Problem 5.8
• Considering the entire beam as a free-body, 
determine the reactions at A and D.
( ) ( )( ) ( )( )
kN0.52
kN50kN60kN0.580
kN0.58
m4kN50m5.1kN60m50
=
−−+==∑
=
−−==∑
y
yy
A
A
AF
D
DM
• Develop the shear diagram and determine the 
maximum bending moment.
( )
kN8
kN60
kN0.52
−=
−=−=−
==
B
AB
yA
V
curveloadunderareaVV
AV
• Maximum bending moment occurs at 
V = 0 or x = 2.6 m.
( )
kN6.67
,max
=
= EtoAcurveshearunderareaM
© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 
MECHANICS OF MATERIALS
Third
Edition
Beer • Johnston • DeWolf
5 - 22
Sample Problem 5.8
• Determine the minimum acceptable beam 
section modulus. 
3336
max
min
mm105.422m105.422
MPa160
mkN6.67
×=×=
⋅==
−
all
M
S σ
• Choose the best standard section which meets 
this criteria.
4481.46W200
5358.44W250
5497.38W310
4749.32W360
63738.8W410
mm, 3
×
×
×
×
×
SShape 9.32360×W
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