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Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and shear stress. To analyze and design members subject to axial load and direct shear. To define normal and shear strain, and show how they can be determined for various types of problems. Copyright © 2011 Pearson Education South Asia Pte Ltd
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Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

Dec 21, 2015

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Page 1: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

Chapter Objectives To show how to use the method of sections for

determining the internal loadings in a member. To introduce the concepts of normal and shear stress. To analyze and design members subject to axial load

and direct shear. To define normal and shear strain, and show how they

can be determined for various types of problems.

Copyright © 2011 Pearson Education South Asia Pte Ltd

Page 2: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

• Reading Quiz• Applications• Normal Stress• Shear Stress• Normal Strain• Shear Strain• Cartesian Strain Components• Concept Quiz

In-Class Activities

Copyright © 2011 Pearson Education South Asia Pte Ltd

Page 3: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

READING QUIZ

1. What is the normal stress in the bar if P=10 kN and 500 mm²?

a) 0.02 kPa

b) 20 Pa

c) 20 kPa

d) 200 N/mm²

e) 20 MPa

Copyright © 2011 Pearson Education South Asia Pte Ltd

Page 4: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

READING QUIZ (cont)

2. What is the average shear stress in the internal vertical surface AB (or CD), if F=20 kN, and AAB=ACD=1000 mm²?

a) 20 N/mm²

b) 10 N/mm²

c) 10 kPa

d) 200 kN/m²

e) 20 MPa

Copyright © 2011 Pearson Education South Asia Pte Ltd

Page 5: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

READING QUIZ (cont)

3. The center portion of the rubber balloon has a diameter of d = 100 mm. If the air pressure within it causes the balloon’s diameter to become d = 125 mm, determine the average normal strain in the rubber.

a) 0.2

b) 0.25 π

c) 0.25

d) 1.25

Copyright © 2011 Pearson Education South Asia Pte Ltd

Page 6: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

READING QUIZ (cont)

4. What is the unit of strain?

a) mm

b) mm/m

c) Micron

d) no unit

Copyright © 2011 Pearson Education South Asia Pte Ltd

Page 7: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

APPLICATIONS

Copyright © 2011 Pearson Education South Asia Pte Ltd

Where does the average normal stress occur?

Page 8: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

Copyright © 2011 Pearson Education South Asia Pte Ltd

Page 9: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

APPLICATIONS (cont)

Copyright © 2011 Pearson Education South Asia Pte Ltd

Will the total shear force over the anchor length be equal to the total tensile force σtensile A in the bar?

Page 10: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

APPLICATIONS

Copyright © 2011 Pearson Education South Asia Pte Ltd

Page 11: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

AVERAGE NORMAL STRESS

Copyright © 2011 Pearson Education South Asia Pte Ltd

Will the total shear force over the anchor length be equal to the total tensile force σtensile A in the bar?

A

P

Page 12: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

NORMAL SHEAR STRESS

Copyright © 2011 Pearson Education South Asia Pte Ltd

A

FzA

z

0

lim

A

FA

F

y

Azy

x

Azx

0

0

lim

lim

Page 13: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 1

Copyright © 2011 Pearson Education South Asia Pte Ltd

The bar in Fig. 7-14a has a constant width of 35 mm and a thickness of 10 mm. Determine the maximum average normal stress in the bar when it is subjected to the loading shown.

Page 14: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 1 (cont)

Copyright © 2011 Pearson Education South Asia Pte Ltd

• Graphically, the normal force diagram is as shown.

• By inspection, different sections have different internal forces.

Solution

Page 15: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 1 (cont)

Copyright © 2011 Pearson Education South Asia Pte Ltd

• By inspection, the largest loading is in region BC,

• Since the cross-sectional area of the bar is constant, the largest average normal stress is

Solution

kN 30BCP

(Ans) MPa 7.85

01.0035.0

1030 3

A

PBCBC

Page 16: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

DESIGN OF SIMPLE CONNECTION

Copyright © 2011 Pearson Education South Asia Pte Ltd

• For normal force requirement

• For shear force requirement

allow

PA

allow

VA

Page 17: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 2

Copyright © 2011 Pearson Education South Asia Pte Ltd

The rigid bar AB shown in Fig. 1–29a is supported by a steel rod AC having a diameter of 20 mm and an aluminum block having a cross sectional area of 1800 mm2. The 18-mm-diameter pins at A and C are subjected to single shear. If the failure stress for the steel and aluminum is and , respectively, and the failure shear stress for each pin is , determine the largest load P that can be applied to the bar. Apply a factor of safety of FS=2.

MPa 680failst MPa 70failal

MPa 900fail

Page 18: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 2 (cont)

Copyright © 2011 Pearson Education South Asia Pte Ltd

• The allowable stresses are

• There are three unknowns and we apply the equations of equilibrium,

Solution

MPa 4502

900

..

MPa 352

70

..

MPa 3402

680

..

SF

SF

SF

failallow

failal

allowal

failst

allowst

(2) 075.02 ;0

(1) 0225.1 ;0

PFM

FPM

BA

ACB

Page 19: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 2 (cont)

Copyright © 2011 Pearson Education South Asia Pte Ltd

• We will now determine each value of P that creates the allowable stress in the rod, block, and pins, respectively.

• For rod AC,

• Using Eq. 1,

• For block B,

• Using Eq. 2,

Solution

kN 8.10601.010340 26 ACallowstAC AF

kN 171

25.1

28.106P

kN 0.631018001035 66 BallowalB AF

kN 168

75.0

20.63P

Page 20: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 2 (cont)

Copyright © 2011 Pearson Education South Asia Pte Ltd

• For pin A or C,

• Using Eq. 1,

• When P reaches its smallest value (168 kN), it develops the allowable normal stress in the aluminium block. Hence,

Solution

kN 5.114009.010450 26 AFV allowAC

kN 183

25.1

25.114P

(Ans) kN 168P

Page 21: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

NORMAL STRAIN

Copyright © 2011 Pearson Education South Asia Pte Ltd

s

ssavg

'

ss 1'

s

ssnAB

'lim

along

Page 22: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

SHEAR STRAIN

Copyright © 2011 Pearson Education South Asia Pte Ltd

'lim2

along along tACnAB

nt

Page 23: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

CARTESIAN STRAIN COMPONENTS

Copyright © 2011 Pearson Education South Asia Pte Ltd

• The approximate lengths of the sides of the parallelepiped are

• The approximate angles between sides, again originally defined by the sides Δ x, Δ y and Δ z are

• Notice that the normal strains cause a change in volume of rectangular element, whereas the shear strain cause a change in shape

zyx zyx 1 1 1

xzyzxy

2

2

2

Page 24: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

CARTESIAN STRAIN COMPONENTS (cont)

Copyright © 2011 Pearson Education South Asia Pte Ltd

Page 25: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 3

Copyright © 2011 Pearson Education South Asia Pte Ltd

The slender rod creates a normal strain in the rod of where z is in meters. Determine (a) displacement of end B due to the temperature increase, and (b) the average normal strain in the rod.

2/131040 zz

Page 26: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 3 (cont)

Copyright © 2011 Pearson Education South Asia Pte Ltd

Part (a)• Since the normal strain is reported at each point along the rod, it has a

deformed length of

• The sum along the axis yields the deformed length of the rod is

• The displacement of the end of the rod is therefore

Solution

dzzdz 2/1310401'

m 20239.010401'2.0

0

2/13 dzzz

(Ans) mm39.2m00239.02.020239.0 B

Page 27: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 3 (cont)

Copyright © 2011 Pearson Education South Asia Pte Ltd

Part (b)• Assumes the rod has an original length of 200 mm and a change in

length of 2.39 mm. Hence,

Solution

(Ans) mm/mm 0119.0200

39.2'

s

ssavg

Page 28: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 4

Copyright © 2011 Pearson Education South Asia Pte Ltd

Due to a loading, the plate is deformed into the dashed shape shown in Fig. 2–6a. Determine (a) the average normal strain along the side AB, and (b) the average shear strain in the plate at A relative to the x and y axes.

Page 29: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 4 (cont)

Copyright © 2011 Pearson Education South Asia Pte Ltd

Part (a)• Line AB, coincident with the y axis, becomes line AB’ after deformation,

thus the length of this line is

• The average normal strain for AB is therefore

• The negative sign indicates the strain causes a contraction of AB.

Solution

mm 018.24832250' 22 AB

(Ans) mm/mm 1093.7240

250018.248' 3

AB

ABABavgAB

Page 30: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

EXAMPLE 4 (cont)

Copyright © 2011 Pearson Education South Asia Pte Ltd

Part (b)Part (b)• As noted, the once 90° angle BAC between the sides of the plate,

referenced from the x, y axes, changes to θ’ due to the displacement of B to B’.

• Since then is the angle shown in the figure.

• Thus,

Solution

'2 xy xy

(Ans) rad 121.02250

3tan 1

xy

Page 31: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

CONCEPT QUIZ

1) The thrust bearing is subjected to the loads as shown. Determine the order of average normal stress developed on cross section through B, C and D.

a) C > B > D

b) C > D > B

c) B > C > D

d) D > B > C

Copyright © 2011 Pearson Education South Asia Pte Ltd

Page 32: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

CONCEPT QUIZ (cont)

2) The rectangular membrane has an un-stretched length L1 and width L2. If the sides are increased by small amounts ΔL1 and ΔL2, determine the normal strain along the diagonal AB.

Copyright © 2011 Pearson Education South Asia Pte Ltd

2

221

22

21

21

21

22

21

22

21

2

2

1

1

D) C)

B) A)

LL

LL

LL

LL

LL

LL

L

L

L

L

Page 33: Chapter Objectives To show how to use the method of sections for determining the internal loadings in a member. To introduce the concepts of normal and.

CONCEPT QUIZ (cont)

3) The rectangular plate is subjected to the deformation shown by the dashed line. Determine the average shear strain γxy of the plate.

Copyright © 2011 Pearson Education South Asia Pte Ltd

22 200150

3

200

150

200

3

150

3

D) C)

B) A)