Problem

Solve Example 15.2 for the condition that d = 200 mm and 2c = 50 mm.Example 15.2 Brittle F...

Solve Example 15.2 for the condition that d = 200 mm and 2c = 50 mm.

Example 15.2 Brittle Fracture for Combined Tension and Bending

A hook similar to that shown in Figure E15.2 is part of a scarifier used to dig up old road beds before replacing them. Let the tool be made of AISI 4340 steel and heat-treated to the properties indicated in Table 15. 1. The dimensions of the tool are as follows: d = 250 mm, 2c = 60 mm, and the width of the rectangular cross section is t = 25 mm. Determine the magnitude of the fracture load P for a crack length of

(a) a = 5 mm and


(b) a = 10 mm.

FIGURE E15.2

Solution:

Note that both the width t and crack length a satisfy Eq. 15.29; therefore, the hook is assumed to be loaded in the brittle state. At a section through the crack, the hook is subjected to combined axial load (Case 4 of Table 15.2) and bending (Case 6 of Table 15.2). Since a linear elastic analysis is assumed, the state of stress for combined loading can be obtained by superposition of the two states of stress for the two types of loading. Thus,

σf(λ) = σ1f1(λ) + σ2f2(λ)

(a) When a = 5 mm, λ = a/2c = 0.083. From Table 15.2 for Cases 4 and 6, we obtain f1(λ) = 1.22 and f2(λ) = 1.02. Therefore,

This is substituted in the relation

t. give

 


(b) When a = 10 mm, λ = 0.167 and

 

Table 15.1:

TABLE 15.1 KIC Critical Stress Intensity Factor (Fracture Toughness)a

Material

σu[MPa]

Y [MPa]

Minimum values for B, a, t [mm]

Alloy Steels

 

 

 

 

A533B

500

175

306.0

2618 Ni Mo V

648

106

66.9

V1233 Ni Mo V

593

75

40.0

124 K 406 Cr Mo V

648

62

22.9

17-7PH

1289

1145

77

11.3

17-4PH

1331

1172

48

4.2

Ph 15-7M0

1600

1413

50

3.1

AISI 4340

1827

1503

59

3.9

Stainless Steel

 

 

 

 

AISI 403

821

690

77

31.1

Aluminum Alloys

 

 

 

 

6061-T651

352

299

29

23.5

2219-T851

454

340

32

22.1

7075-T7351

470

392

31

15.6

7079-T651

569

502

26

6.7

2024-T851

488

444

23

6.7

Titanium Alloys

 

 

 

 

Ti-6AI-4Zr-2Sn-0.5Mo-0.5V

890

836

139

69.1

Ti-6AI-4V-2Sn

852

798

111

48.4

Ti-6.5AI-5Zr-1V

904

858

106

38.2

Ti-6AI-4Sn-1V

889

878

93

28.0

Ti-6AI-6V-2.5Sn

1176

1149

66

8.2

aRoom temperature data.

 (15.29)

Case 4 of Table 15.2:

TABLE 15.2 Stress Intensity Factors KI

Case 4: Single-edge crack in finite-width sheet

λ

f(λ)

0(c → ∞)

1.12

0.2

1.37

0.4

2.11

0.5

2.83

Case 6 of Table 15.2:

TABLE 15.2 Stress Intensity Factors KI

Case 6: Edge crack in beam in bending

λ

f(λ)

0.1

1.02

0.2

1.06

0.3

1.16

0.4

1.32

0.5

1.62

0.6

2.10

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