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 3/8/2015 1  h  i     r   d  E  d  i      t    i      o n Beer • Johnston • DeWolf  Analysis and Design of Beams for Bending Introduction Shear and Bending Moment Diagrams   . 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. 5 - 1  h  i     r   d  E  d  i      t    i      o n Beer • Johnston • DeWolf Introduction  Beams - structural members supporting loads at various points along the member Object ive - Analys is and desi gn of beams Transvers e loadings of bea ms are classi fied as concentrated loads or distributed loads Applie d loads result in inte rnal forces consisti ng of a shear force (from the shear stress distribution) and a bending couple (from the normal stress distribution) © 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 - 2 Normal st ress is ofte n the critic al design cr iteria S  M  I c  M  I  My m  x        Requires determination of the location and magnitude of largest bending moment  MECHANICS OF MATERIAL S T h  i     r   d  E  d  i      t    i      o n Beer • Johnston • DeWolf Introduction Classification of Beam Supports © 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 - 3  MECHANICS OF MATERIAL S T h  i     r   d  E  d  i      t    i      o n Beer • Johnston • DeWolf Shear and Bending Moment Diagrams Determination of maxi mum normal and shearing stresses requires identification of maximum internal shear force and bending couple. Shear force and be nding couple at a poi nt are determined by passing a section through the  beam and applying an e quilibrium analysis on the beam portions on either side of the section. Si n conventi ons for shear f orce s V and V’ © 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 - 4 and bending couples M and M’

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3/8/2015

1

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Beer • Johnston • DeWolf 

 Analysis and Design of Beams for Bending

Introduction

Shear and Bending Moment Diagrams

 

.

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. 5 - 1

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Beer • Johnston • DeWolf 

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)

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 - 2

• Normal stress is often the critical design criteria

 M 

 I 

c M 

 I 

 Mym x         

Requires determination of the location and

magnitude of largest bending moment

MECHANICS OF MATERIALST h  i     r   d  

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Beer • Johnston • DeWolf 

Introduction

Classification of Beam Supports

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 - 3

MECHANICS OF MATERIALST h  i     r   d  

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Beer • Johnston • DeWolf 

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.

• Si n conventions for shear forces V and V’

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 - 4

and bending couples M and M’

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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 a l e uilibrium 

analyses on resulting free-bodies.

ftkip5.1030

kips3030

:

2

21

1    

 

 x M  M  x x M 

 xV V  xF 

C to AFrom

 y

:

 DtoC From

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 - 9

ftkip2496042402       x M  M  x M 

 y

ftkip34226kips34

:

  x M V 

 Bto DFrom

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Beer • Johnston • DeWolf 

Sample Problem 5.2

• Apply the elastic flexure formulas to

determine the maximum normal stress tothe left and right of point D.

 

shape, S = 126 in3 about the X-X axis.

3

inkip1776

:

in126

inkip2016

:

 M 

 Dof right theTo

 M 

 Dof left theTo

m

  

   ksi0.16m  

ksi1.14m  

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 -10

in126S 

MECHANICS OF MATERIALST h  i     r   d  

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Relations Among Load, Shear, and Bending Moment

 xwV 

 xwV V V F  y

0:0

• Relationship between load and shear:

 D

 x

 xC  D   dxwV V 

wdx

0:0  x

 xw xV  M  M  M  M C   

 

• Relationship between shear and bending

moment:

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 -11

221  xw xV  M   

 D

 x

 xC  D   dxV  M  M 

dx

dM 0

MECHANICS OF MATERIALST h  i     r   d  

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Sample Problem 5.3

SOLUTION:

• Taking the entire beam as a free body,

determine the reactions at A and D.

Draw the shear and bending

moment diagrams for the beam

and loading shown.

• Apply the relationship between shear and load

to develop the shear diagram.

• Apply the relationship between bending

moment and shear to develop the bending

moment diagram.

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 -12

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Sample Problem 5.3

SOLUTION:

• Taking the entire beam as a free body, determine the

reactions at A and D.

0 M 

kips18

kips12kips26kips12kips200

0F

kips26

ft28kips12ft14kips12ft6kips20ft240

y

 y

 y

 A

 A

 D

 D

• Apply the relationship between shear and load to

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 -13

develop the shear diagram.

dxwdV wdx

dV 

- zero slope between concentrated loads

- linear variation over uniform load segment

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Sample Problem 5.3

• Apply the relationship between bending moment

and shear to develop the bending momentdiagram.

dM 

dx

- bending moment at A and E is zero

- 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. 5 -14

- 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

MECHANICS OF MATERIALST h  i     r   d  

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Sample Problem 5.5

SOLUTION:

• Taking the entire beam as a free body,

determine the reactions at C .

Draw the shear and bending moment

diagrams for the beam and loading

shown.

• Apply the relationship between shear and

load to develop the shear diagram.

• Apply the relationship between bending

moment and shear to develop the bending

moment diagram.

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 -15

MECHANICS OF MATERIALST h  i     r   d  

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Beer • Johnston • DeWolf 

Sample Problem 5.5

SOLUTION:

• Taking the entire beam as a free body, determine

the reactions at C .

11

 

  

 

 

  

 

330 02

102

1

22

a Law M  M 

a Law M  C C C 

 y

Results from integration of the load and shear

distributions should be equivalent.

• Apply the relationship between shear and load to

develop the shear diagram.

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 -16

curveload under areaawV 

a

 x xwdx

a

 xwV V 

 B

aa

 A B

 

 

 

   

 

  

 

021

0

2

00

02

1

- No change in shear between B and C.

- Compatible with free body analysis

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Sample Problem 5.5

• Apply the relationship between bending moment and

shear to develop the bending moment diagram.

322  x x xa

a            

203

1

0

00

0622

aw M 

awdx

a xw M  M 

 B

 A B

 

  

 

 

   

 

 

   

  

 

 

323 0

061

021

021

a L

waa Law M 

a Lawdxaw M  M 

 L

aC  B

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 -17

Results at C are compatible with free-body

analysis

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Design of Prismatic Beams for Bending

• The largest normal stress is found at the surface where the

maximum bending moment occurs.

 M c M m

maxmax   

• 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.

allm

 M 

    

max

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 -18

• 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.

all  

m n

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Sample Problem 5.8

SOLUTION:

• Considering the entire beam as a free-

 body, determine the reactions at A and D.

A simply supported steel beam is tocarry 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

• Develop the shear diagram for the beam

and load distribution. From thediagram, determine the maximum

 bending moment.

• Determine the minimum acceptable

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 -19

- . eam sect on mo u us. oose t e est

standard section which meets this

criteria.

MECHANICS OF MATERIALST h  i     r   d  

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Sample Problem 5.8

• Considering the entire beam as a free-body,

determine the reactions at A and D.

kN0.58

m4kN50m5.1kN60m50

  A

 D

 D M 

kN0.52

kN50kN60kN0.580

 y

 y y

 A

 AF 

• Develop the shear diagram and determine the

maximum bending moment.

kN60

kN0.52

 A B

 y A

curveload under areaV V 

 AV 

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 -20

 B

• Maximum bending moment occurs at

V = 0 or x = 2.6 m.

kN6.67

,max

  E to Acurveshear under area M 

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Sample Problem 5.8

• Determine the minimum acceptable beam section

modulus.

maxmin

MPa160

mkN6.67  

 M S 

  

3336mm105.422m105.422    

a

• Choose the best standard section which meets this

criteria.

63738.8W410

mm,3

S Shape   9.32360W 

© 2002 The McGraw-Hill Companies, Inc. All rights reserved. 5 -21

4481.46W200

5358.44W250

5497.38W310

4749.32W360

MECHANICS OF

MATERIALS

Third Edition

CHAPTER

Ferdinand P. Beer 

E. Russell Johnston, Jr.

John T. DeWolf 

Lecture Notes:

J. Walt Oler 

 Analysis and Design

of Beams for Bending

Texas Tech University

© 2002 The McGraw-Hill Companies, Inc. All rights reserved.