Mechanics & Materials 1 Chapter 14 Combined Loadings

28
- Mechanics & Materials 1 FAMU FSU College of Engineering Department of Mechanical Engineering Chapter 14 Chapter 14 Combined Loadings Combined Loadings

Transcript of Mechanics & Materials 1 Chapter 14 Combined Loadings

Page 1: Mechanics & Materials 1 Chapter 14 Combined Loadings

-

Mechanics & Materials 1

FAMU FSU College of Engineering

Department of Mechanical Engineering

Chapter 14 Chapter 14

Combined LoadingsCombined Loadings

Page 2: Mechanics & Materials 1 Chapter 14 Combined Loadings

Thin Walled Pressure VesselsThin Walled Pressure Vessels

• Cylindrical or spherical pressure vessels are used in industry as tanks, boilers or containers.

• When under pressure the material is subjected to loadings in all directions.

• In general thin wall refers to an inner radius to wall thickness ratio ri/t ≥ 10, in most cases it is actually > 50.

• If the vessels wall is thin, the stress distribution through thethickness can be assumed to be uniform or constant.

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Cylindrical Pressure VesselsCylindrical Pressure Vessels

• Consider tubes with an internal pressure and closed ends

• σxx �axial stress due to the pressure on the end walls

• σθθ�“Hoop” stress due to

the pressure acting on the curved surface.

• P is the internal pressure• Look at a FBD of the axial

section

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Axial Stress

• Consider the axial equilibrium on this structure.

• Which gives the equation for Axial Stress:

( ) 2

2

2*

20

rPrt

rtrPF

xx

xxx

ππσ

σππ

=

+−==∑

txx 2

Pr2 == σσ

Cylindrical Pressure Vessels: Cylindrical Pressure Vessels: Axial StressAxial Stress

Page 5: Mechanics & Materials 1 Chapter 14 Combined Loadings

Look now at a FBD of the circumferential section

• Equating the forces vertically gives:

• Which simplifies to give the equation for Hoop Stress:

Cylindrical Pressure Vessels: Cylindrical Pressure Vessels: Hoop StressHoop Stress

t

pr== 1σσθθ

rLPLt

LtLRPFy

2)(2

2*2**0

=

+−==∑θθ

θθ

σσ

Page 6: Mechanics & Materials 1 Chapter 14 Combined Loadings

Cylindrical Pressure VesselsCylindrical Pressure Vessels

• Pressure vessels also have stresses created by the weight of the pressurized fluid inside, its own weight, externally applied loads and by an applied torque.

• To analyze this, each loading condition is analyzed individually and the stresses are then combined along their respective axes by the superposition method.

• Pressure vessel with ALL possible loading conditions:

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Pressure Vessel With ALL Pressure Vessel With ALL Possible Loading Conditions:Possible Loading Conditions:

Page 8: Mechanics & Materials 1 Chapter 14 Combined Loadings

Spherical Pressure VesselsSpherical Pressure Vessels

• Common for storing liquid gases (maximum storage volume for the least volume of material)

• Equating the forces vertically:

• Which simplifies to:

• This is not dependent on the orientation of our FBD, so this stress acts on both surfaces of the element simultaneously.

∑ +−== σππ rtrPFy 2*0 2

t2

Pr=σ

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Example Example

• A steel gas bottle 2 m long with a diameter of 250 mm and a 3 mm wall thickness is pressurized to 3 MPa.

• Determine the stresses

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SolutionSolution

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Problem 14.1Problem 14.1

• The spherical gas tank has an inner radius of r = 1.5m.(If it is subjected to an internal pressure of p=300kPa, determine its required thickness if the maximum normal stress is not to exceed 12 MPa.

Page 12: Mechanics & Materials 1 Chapter 14 Combined Loadings

mmmtt

tallowz

8.1801875.0 2

)5.1)(10(300)10(12

2

Pr

36

==

=

== σσ

SolutionSolution

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Example 14.3Example 14.3

• The cap of the cylindrical tank is bolted along the flanges. The tank has an inner diameter of 1.5m and a wall thickness of 18mm.

• If the largest normal stress is not to exceed 150MPa, determine the maximum pressure the tank can sustain .

• Also compute the number of bolts required to attach the cap to the tank if each bolt has a diameter of 20mm.

• The allowable stress for the bolt is 180MPa

Page 14: Mechanics & Materials 1 Chapter 14 Combined Loadings

MPam

N

t

r

60.3000,600,3

018.0

)75.0()150(10

0.759mr here

2

6

1

==

=

==

ρ

ρ

ρσ

1135.112

)02.0)(4/(

)10(73.6361)10(180

73.6361

)5.1)(4/)(10(60.3

2

36

26

⇒=

=

=

=

==

n

n

nA

F

kN

FF

b

ballow

bpr

π

σ

π

Fpr Fb

SolutionSolution

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Analysis of Stress in Combined LoadingAnalysis of Stress in Combined Loading

• Normal Stress Sources( σ)– Axial Load :- The uniform normal stress distribution due to the normal

force.

– Bending Moment :- Normal stress distribution due to the bending moment.

– Pressure Cylinder :- Biaxial state of stress in the material due to pressure in a thin-walled cylinder.

– Thermal :- Normal stress distribution due to temperature change.

A

F=σ

I

My=σ

t

pr=σ 1t

pr

22=σ

TE∆= ασ

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• Shear Stress Sources (τ):– Torsion:- Shear-stress distribution that varies linearly from the

central axis to the maximum at the shaft’s outer boundary.

– Transverse Shear Stress :- Shear stress distribution that acts over the cross section.

Analysis of Stress in Combined Analysis of Stress in Combined LoadingLoading

J

T ρτ =

It

VQ=τ

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Analysis of Stress in Combined Analysis of Stress in Combined LoadingLoading

• After finding each component of the stress we– add (algebraically) all those components which

contribute normal stress to get the total normal stress– add (algebraically) the components which give a shear

stress to get the total shear stress. – We can’t add a shear component to a normal stress

component, because stresses are tensorial quantities which need at least 2 directions rather than one as in the vectors.

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Analysis of Stress in Combined Analysis of Stress in Combined LoadingLoading

Remember to assign positive or negative signs for the stresses according to

• Axial Loading σ + (tension), σ(-) compression• Bending: σ sign depends on both M sign and c sign, M

sign from Moment diagram, c sign from N.A location• Pressure: Inside pressure σ +, outside pressureσ -• Thermal: Heating: expansion +σ, cooling: contraction: -σ• Torsion: τ sign depends on torque (T) sign (Right hand

rule)• Transverse Shear: τ sign depends on Q sign (N.A location

and section of interest) and shear force sign V, from shear diagram)

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Combined LoadingCombined Loading• This example has multiple stress

components. The stresses on the rod are axial, shear, two bending, and a torsional stress.

• NOTE THAT ONLY 2 LOADS LEADS TO 5 STRESS COMPONENTS !!

• When found, each stress value is understood as shown in the diagram below.

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Problem 14.11Problem 14.11

• The offset link supports the loading shown. Determine its required width w if the allowable normal stress is 73MPa. The link thickness is 40mm.

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σ due to axial force

σ due to bending

wwA

Pa

)10(750

)04.0(

)10(30 33

===σ

2

3

3

3

205.0)10(4500

))(04.0(121

2205.0)10(30

w

w

w

ww

I

Mcb

+=

+==σ

baallow σσσσ +==max

SolutionSolution

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mm

mw

ww

www

w

w

w

7.79

0797.0

0225.0373

25.2225.075.073

205.0)10(4500

)10(750)10(73

2

2

2

33

6

==

=−−

++=

++=

SolutionSolution

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Problem 14.20Problem 14.20

• The bar has a diameter of 40mm. If it is subjected to a force of 800N as shown, determine the stress components that act at points A and B and show results on volume elements located at these points.

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MPa

I

Mz

A

P

m

AyQ

rA

m

rI

A

A

318.0

0)10(256637.1

400

Bending extension Axial :stress Axial

0Q

)10(3333.5

2

)02.0(

3

)02.0(4

)10(256637.1

)02.0(

)10(1256637.0

)02.0)((4

1

4

1

3

B

36

2

3

22

46

44

=

+=+=

+=

=

=′′=

===

=

==

σ

ππ

ππ

ππ

SolutionSolution

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0

7.21

)10(1256637.0

)02.0(56.138

)10(1256637.0

400

735.0

)04.0)(10(1256637.0

)10)(3333.5(82.692

66

6

6

=−=

−=−=

=

==

−−

B

B

AA

MPa

I

Mc

A

P

MPa

It

VQ

τ

σ

τ

SolutionSolution

Shear Stress: Only transverse shear

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Problem 14.25Problem 14.25

• The pliers are made from two steel parts pinned together at A.

• If a smooth bolt is held in the jaws and a gripping force of 10lb is applied at the handles, determine the stress components in the pliers at points B and C.

• The cross section is rectangular having dimensions as shown.

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lbM

F

lbV

F

c

y

X

30

010(3)-M 0M

5lbN

010sin30-N 0

660.8

010cos30-V 0

=

===

===

==

0

)10(4

)2.0)(2.0)(1.0(

)10(0667.1

)4.0)(2.0(12

1

33

3

3

==

=′′==

=

B

c

Q

in

AyQ

I

SolutionSolution

xx

yy

BB

0.40.4””

0.20.2””

CC

__yy’’ =.1=.1””

208.0)4.0(2.0 inA ==

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ksi

psi

I

M

A

N yB

56.5

5562

)10(0666.1

)2.0(30

08.0

53

==

−=+−= −σ

psiIt

VQ

psiI

M

A

N

cc

yc

B

162)2.0)(10(0667.1

)10)(4(660.8

5.6208.0

5

0

3

3

===

−=−=+−=

=

τ

σ

τ

BB

0.4”0.4”

0.2”

0.2”

__y’=.1”y’=.1”

SolutionSolution

N.AN.A