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Lecture Mechanics of materials (Third edition) - Chapter 6: Shearing stresses in beams and thinwalled members

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• Determine the horizontal force per unit length or shear flow q on the lower surface of the upper plank. • Calculate the corresponding shear[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

Shearing Stresses in

Beams and Thin-Walled Members

Trang 2

Thin-Walled Members

Introduction

Shear on the Horizontal Face of a Beam Element

Example 6.01

Determination of the Shearing Stress in a Beam

Shearing Stresses τxy in Common Types of Beams

Further Discussion of the Distribution of Stresses in a

Sample Problem 6.2

Longitudinal Shear on a Beam Element of Arbitrary Shape

Example 6.04

Shearing Stresses in Thin-Walled Members

Plastic Deformations

Sample Problem 6.3

Unsymmetric Loading of Thin-Walled Members

Example 6.05

Example 6.06

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0

0

0 0

=

∫ −

=

=

=

=

=

=

=

=

=

=

=

x z

xz z

x y

xy y

xy xz

x x

x

y M

dA F

dA z

M V

dA F

dA z

y M

dA F

σ τ

σ τ

τ τ

σ

• Distribution of normal and shearing stresses satisfies

• Transverse loading applied to a beam results in normal and shearing stresses in transverse sections

• When shearing stresses are exerted on the vertical faces of an element, equal stresses must be exerted on the horizontal faces

• Longitudinal shearing stresses must exist

in any member subjected to transverse loading

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• Consider prismatic beam

• For equilibrium of beam element

=

∑ = = ∆ + ∫ −

A

C D

A

D D

x

dA y I

M M

H

dA H

x V x dx

dM M

M

dA y Q

C D

A

=

=

=

• Note,

flow

shear I

VQ x

H q

x I

VQ H

=

=

=

=

• Substituting,

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Shear on the Horizontal Face of a Beam Element

flow shear

I

VQ x

H

=

• Shear flow,

• where

section cross

full of moment second

above area

of moment first

' 2

1

=

=

=

=

+A A

A

dA y I

y

dA y Q

• Same result found for lower area

Q Q

q I

Q V x

H q

=

=

=

′ +

=

=

=

axis neutral to

respect

h moment wit first

0

Trang 6

• Determine the horizontal force per

unit length or shear flow q on the

lower surface of the upper plank

• Calculate the corresponding shear force in each nail

A beam is made of three planks,

nailed together Knowing that the

spacing between nails is 25 mm and

that the vertical shear in the beam is

V = 500 N, determine the shear force

in each nail

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Example 6.01

4 6

2

3 12

1

3 12

1

3 6

m 10 20 16

] m 060 0 m 100 0 m 020 0

m 020 0 m 100 0 [ 2

m 100 0 m 020 0

m 10 120

m 060 0 m 100 0 m 020 0

×

=

× +

+

=

×

=

×

=

=

I

y A Q

SOLUTION:

• Determine the horizontal force per

unit length or shear flow q on the

lower surface of the upper plank

m

N 3704

m 10 16.20

) m 10 120 )(

N 500 (

4 6

-3 6

=

×

×

=

I

VQ q

• Calculate the corresponding shear force in each nail for a nail spacing of

25 mm

m N q

F = ( 0 025 m ) = ( 0 025 m )( 3704

N 6 92

=

F

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• The average shearing stress on the horizontal

face of the element is obtained by dividing the shearing force on the element by the area of the face

It VQ

x t

x I

VQ A

x q A

H

ave

=

=

=

=

τ

• On the upper and lower surfaces of the beam,

τyx= 0 It follows that τxy= 0 on the upper and lower edges of the transverse sections

• If the width of the beam is comparable or large

relative to its depth, the shearing stresses at D1 and D2 are significantly higher than at D.

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Shearing Stresses τxy in Common Types of Beams

• For a narrow rectangular beam,

A V

c

y A

V Ib

VQ

xy

2 3

1 2

3

max

2 2

=

=

=

τ τ

• For American Standard (S-beam) and wide-flange (W-beam) beams

web

ave

A V It VQ

=

=

max

τ τ

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Stresses in a Narrow Rectangular Beam

=

2

2 1

2

3

c

y A

P

xy

τ

I

Pxy

x = +

σ

• Consider a narrow rectangular cantilever beam

subjected to load P at its free end:

• Shearing stresses are independent of the distance from the point of application of the load

• Normal strains and normal stresses are unaffected

by the shearing stresses

• From Saint-Venant’s principle, effects of the load application mode are negligible except in immediate vicinity of load application points

• Stress/strain deviations for distributed loads are negligible for typical beam sections of interest

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