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Lecture Mechanics of materials (Third edition) - Chapter 7: Transformations of stress and strain

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Application of Mohr’s Circle to the Three- Dimensional Analysis of Stress Yield Criteria for Ductile Materials Under Plane Stress. Fracture Criteria for Brittle Materials Under Plane St[r]

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MECHANICS OF MATERIALS

Ferdinand P Beer

E Russell Johnston, Jr.

John T DeWolf

Lecture Notes:

J Walt Oler Texas Tech University

CHAPTER

Transformations of

Stress and Strain

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Introduction Transformation of Plane Stress Principal Stresses

Maximum Shearing Stress Example 7.01

Sample Problem 7.1 Mohr’s Circle for Plane Stress Example 7.02

Sample Problem 7.2 General State of Stress Application of Mohr’s Circle to the Three- Dimensional Analysis of Stress Yield Criteria for Ductile Materials Under Plane Stress

Fracture Criteria for Brittle Materials Under Plane Stress Stresses in Thin-Walled Pressure Vessels

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• The most general state of stress at a point may

be represented by 6 components,

) ,

,

: (Note

stresses shearing

, ,

stresses normal

, ,

xz zx

zy yz

yx xy

zx yz xy

z y x

τ τ

τ τ

τ τ

τ τ τ

σ σ σ

=

=

=

• Same state of stress is represented by a different set of components if axes are rotated

• The first part of the chapter is concerned with how the components of stress are transformed under a rotation of the coordinate axes The second part of the chapter is devoted to a similar analysis of the transformation of the components of strain

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• Plane Stress - state of stress in which two faces of

the cubic element are free of stress For the illustrated example, the state of stress is defined by

0 ,

σ

• State of plane stress occurs in a thin plate subjected

to forces acting in the midplane of the plate

• State of plane stress also occurs on the free surface

of a structural element or machine component, i.e.,

at any point of the surface not subjected to an

Trang 5

( ) ( )

( θ) θ τ ( θ) θ σ

θ θ

τ θ θ

σ τ

θ θ

τ θ θ

σ

θ θ

τ θ θ

σ σ

sin sin

cos sin

cos cos

sin cos

0

cos sin

sin sin

sin cos

cos cos

0

A A

A A

A F

A A

A A

A F

xy y

xy x

y x y

xy y

xy x

x x

∆ +

∆ +

=

=

=

=

• Consider the conditions for equilibrium of a prismatic element with faces perpendicular to

the x, y, and x’ axes.

θ τ

θ σ

σ τ

θ τ

θ σ

σ σ

σ σ

θ τ

θ

σ σ

σ

σ σ

2 cos 2

sin

2 sin 2

cos 2

2

2 sin 2

cos 2

2

• The equations may be rewritten to yield

Trang 6

• The previous equations are combined to yield parametric equations for a circle,

2 2

2 2

2

2 2

where

xy y

x y

x ave

y x ave

x

R

R

τ σ

σ σ

σ σ

τ σ

σ

+

⎟⎟

⎜⎜

=

+

=

= +

• Principal stresses occur on the principal planes of stress with zero shearing stresses

2 2

min max,

2 2

tan

2 2

y x

xy p

xy y

x y

x

σ σ

τ θ

τ σ

σ σ

σ σ

=

+

⎟⎟

⎜⎜

± +

=

Trang 7

Maximum shearing stress occurs for σx′ = σave

2

45

by from

offset

and 90

by separated angles

two defines :

Note

2 2

tan

2

o

o

2 2 max

y x

ave

p

xy

y x

s

xy y

x

R

σ

σ σ

σ

θ

τ

σ σ

θ

τ σ

σ τ

+

=

=

=

+

⎟⎟

⎜⎜

=

=

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For the state of plane stress shown,

determine (a) the principal panes,

(b) the principal stresses, (c) the

maximum shearing stress and the

corresponding normal stress

SOLUTION:

• Find the element orientation for the principal stresses from

y x

xy

τ θ

= 2 2

tan

• Determine the principal stresses from

2

2 min

max,

2

y x

y

σ

⎜⎜

⎛ −

±

+

=

• Calculate the maximum shearing stress with

2

2 max

y

σ

⎜⎜

⎛ −

=

y

σ

σ′ = +

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• Find the element orientation for the principal stresses from

( ) ( )

°

°

=

=

+

=

=

1 233 , 1 53 2

333

1 10 50

40 2

2 2

tan

p

y x

xy p

θ

σ σ

τ θ

°

°

= 26 6 , 116 6

p

θ

MPa 10

MPa 40

MPa 50

=

+

= +

=

x

xy x

σ

τ σ

• Determine the principal stresses from

( ) ( )2 2

2

2 min

max,

40 30

20

2 2

+

±

=

+

⎟⎟

⎜⎜

⎛ −

±

+

x σ y σx σy τxy σ

MPa 70

max =

σ

Trang 10

MPa 10

MPa 40

MPa 50

=

+

= +

=

x

xy x

σ

τ σ

• Calculate the maximum shearing stress with

( ) ( )2 2

2

2 max

40 30

2 +

=

+

⎟⎟

⎜⎜

⎛ −

= σx σ y τxy τ

MPa 50

max =

τ

45

θ

°

°

= 18 4 , 71 6

s

θ

2

10 50 2

=

+

=

=

ave

σ

σ σ

σ

• The corresponding normal stress is

MPa 20

=

σ

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