01.11.2021 Views

Timothy A. Philpot - Mechanics of materials _ an integrated learning system-John Wiley (2017)

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

The choice of either Equation (12.3) or Equation (12.5) to calculate the normal stress acting

on the inclined plane is a matter of personal preference.

The shear stress τ nt acting on the n face in the t direction can be computed from

Equation (12.4):

2 2

τ =−( σ − σ )sinθcos θ + τ (cos θ − sin θ)

nt x y xy

2 2

=−[(16 MPa) − (42 MPa)]sin58° cos58 °+ ( − 50MPa)[cos 58° − sin 58] °

= 33.6 MPa

Alternatively, Equation (12.6) may be used:

τ

nt

σx

− σ y

=− sin2θ + τxy

cos2θ

2

(16MPa) − (42 MPa)

=−

sin2(58 ° ) + ( − 50MPa) cos2(58 ° )

2

= 33.6 MPa

n

To complete the problem, the stresses acting on the inclined plane are shown in a

sketch. Since σ n is negative, the normal stress acting in the n direction is shown as a

compressive stress. The positive value of τ nt indicates that the stress arrow points in

the positive t direction on the positive n face. The arrows are labeled with the stress

magnitude (i.e., absolute value). The signs associated with the stresses are indicated

by the directions of the arrows.

t

58°

10.24 MPa

33.6 MPa

ExAmpLE 12.4

The stresses shown act at a point on the free surface of a machine

component. Determine the normal stresses σ x and σ y and the shear

stress τ xy at the point.

Plan the Solution

The stress transformation equations are written in terms of σ x , σ y ,

and τ xy ; however, the x and y directions do not necessarily have to be

the horizontal and vertical directions, respectively. Any two orthogonal

directions can be taken as x and y, as long as they define a righthand

coordinate system. To solve this problem, we will redefine the x

and y axes, aligning them with the rotated element. The faces of the

unrotated element will be redefined as the n and t faces.

σy

τxy

σx

20°

28 ksi

42 ksi

66 ksi

SolutioN

Redefine the x and y directions, aligning them with the rotated element.

The axes of the unrotated element will be defined as the n and

t directions.

Accordingly, the stresses acting on the rotated element are now

defined as

σ

σ

τ

x

y

xy

= 66 ksi

=−28 ksi

= 42 ksi

t

σ y

τ xy

n

σ x

20°

28 ksi

42 ksi

y

x

66 ksi

495

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!