Question 9.4: Perform an adequacy assessment of the statically loaded weld...

Perform an adequacy assessment of the statically loaded welded cantilever carrying 500 lbf depicted in Fig. 9–20. The cantilever is made ofAISI 1018 HR steel and welded with a \frac {3}{8}-in fillet weld as shown in the figure. An E6010 electrode was used, and the design factor was 3.0.
(a) Use the conventional method for the weld metal.
(b) Use the conventional method for the attachment (cantilever) metal.
(c) Use a welding code for the weld metal.

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(a) From Table 9–3, S_{y} = 50  kpsi, S_{ut} = 62  kpsi. From Table 9–2, second pattern, b = 0.375 in, d = 2 in, so

A = 1.414hd = 1.414(0.375)2 = 1.06  in^{2}
I_{u} = d^{3}/6 = 2^{3}/6 = 1.33  in^{3}
I = 0.707hI_{u} = 0.707(0.375)1.33 = 0.353  in^{4}

Table 9–2    Bending Properties of Fillet Welds*

Unit Second Moment of Area Location of G Throat Area Weld
I_{u} =\frac {d^{3}}{12} \overline { x}=0

\overline { y}=d/2

A= 0.707hd
I_{u} =\frac {d^{3}}{6} \overline { x}=b/2

\overline { y}=d/2

A= 1.414hd
I_{u} =\frac {bd^{2}}{2} \overline { x}=b/2

\overline { y}=d/2

A= 1.414hd
I_{u} =\frac {d^{2}}{12}(6b + d ) \overline{x} =\frac {b^{2}}{2b + d}

\overline { y}=d/2

A= 0.707h(2b + d)
I_{u} =\frac {2d^{3}}{3} − 2d^{2}\overline{y} + (b + 2d ) \overline{y}^{2} \overline { x}=b/2

\overline { y}=\frac {d^{2}}{b+2d}

A= 0.707h(b + 2d)
I_{u} =\frac {d^{2}}{6}(3b + d ) \overline { x}=b/2

\overline { y}=d/2

A= 1.414h(b+ d)
I_{u} =\frac {2d^{3}}{3} − 2d^{2}\overline{y} + (b + 2d ) \overline{y}^{2} \overline { x}=b/2

\overline { y}=\frac {d^{2}}{b+2d}

A = 0.707h(b+ 2d)
I_{u} =\frac {d^{2}}{6}(3b + d ) \overline { x}=b/2

\overline { y}=d/2

A = 1.414h(b + d)
l_{u }= πr^{3} A =1.414πhr

*I_{u}, unit second moment of area, is taken about a horizontal axis through G, the centroid of the weld group, h is weld size; the plane of the bending couple is normal to the plane of the paper and parallel to the y-axis; all welds are of the same size.

Table 9–3   Minimum Weld-Metal Properties

Percent Elongation Yield Strength, psi (MPa) Tensile Strength kpsi (MPa) AWS Electrode Number*
17–25 50 (345) 62 (427) E60xx
22 57 (393) 70 (482) E70xx
19 67 (462) 80 (551) E80xx
14-17 77 (531) 90 (620) E90xx
13-16 87 (600) 100 (689) E100xx
14 107 (737) 120 (827) E110xx

*The American Welding Society (AWS) specification code numbering system for electrodes. This system uses an E prefixed to a fouror five-digit numbering system in which the first two or three digits designate the approximate tensile strength. The last digit includes variables in the welding technique, such as current supply. The next-to-last digit indicates the welding position, as, for example, flat, or vertical, or overhead. The complete set of specifications may be obtained from the AWS upon request.

 

Primary shear:

τ^{′}=\frac {F}{A} =\frac {500(10^{−3})}{1.06} = 0.472  kpsi

Secondary shear:

τ^{″} =\frac {Mr}{I} =\frac {500(10^{−3})(6)(1)}{0.353} = 8.50 kpsi

The shear magnitude τ is the Pythagorean combination

τ = (τ^{′2} + τ^{″2})^{1/2} = (0.4722 + 8.502)^{1/2} = 8.51 kpsi

The factor of safety based on a minimum strength and the distortion- energy criterion is

n =\frac {S_{sy}}{τ} =\frac {0.577(50)}{8.51} = 3.39

Since n ≥ n_{d} , that is, 3.39 ≥ 3.0, the weld metal has satisfactory strength.

(b) From Table A–20, minimum strengths are S_{ut} = 58 kpsi and S_{y} = 32 kpsi.

Table A–20   Deterministic ASTM Minimum Tensile and Yield Strengths for Some Hot-Rolled (HR) and Cold-Drawn (CD) Steels [The strengths listed are estimated ASTM minimum values in the size range 18 to 32 mm ( \frac {3}{4}  to 1\frac {1}{4}in). These strengths are suitable for use with the design factor defined in Sec. 1–10, provided the materials conform to ASTM A6 or A568 requirements or are required in the purchase specifications. Remember that a numbering system is not a specification.] Source: 1986 SAE Handbook, p. 2.15

8

Brinell Hardness

7

Reduction in Area, %

6

Elongation in 2 in, %

5

Yield Strength, MPa (kpsi)

4

Tensile Strength, MPa (kpsi)

3

Proces-sing

2

SAE and/or AISI No.

1

UNS No.

86 55 30 170 (24) 300 (43) HR 1006 G10060
95 45 20 280 (41) 330 (48) CD
95 50 28 180 (26) 320 (47) HR 1010 G10100
105 40 20 300 (44) 370 (53) CD
101 50 28 190 (27.5) 340 (50) HR 1015 G10150
111 40 18 320 (47) 390 (56) CD
116 50 25 220 (32) 400 (58) HR 1018 G10180
126 40 15 370 (54) 440 (64) CD
111 50 25 210 (30) 380 (55) HR 1020 G10200
131 40 15 390 (57) 470 (68) CD
137 42 20 260 (37.5) 470 (68) HR 1030 G10300
149 35 12 440 (64) 520 (76) CD
143 40 18 270 (39.5) 500 (72) HR 1035 G10350
163 35 12 460 (67) 550 (80) CD
149 40 18 290 (42) 520 (76) HR 1040 G10400
170 35 12 490 (71) 590 (85) CD
163 40 16 310 (45) 570 (82) HR 1045 G10450
179 35 12 530 (77) 630 (91) CD
179 35 15 340 (49.5) 620 (90) HR 1050 G10500
197 30 10 580 (84) 690 (100) CD
201 30 12 370 (54) 680 (98) HR 1060 G10600
229 25 10 420 (61.5) 770 (112) HR 1080 G10800
248 25 10 460 (66) 830 (120) HR 1095 G10950

Then

σ =\frac {M}{I/c} =\frac {M}{bd^{2}/6} =\frac {500(10^{−3})6}{0.375(2^{2})/6} = 12  kpsi
n =\frac {S_{y}}{σ} =\frac {32}{12} = 2.67

Since n < n_{d}, that is, 2.67 < 3.0, the joint is unsatisfactory as to the attachment strength.

(c) From part (a), τ = 8.51 kpsi. For an E6010 electrode Table 9–6 gives the allowable shear stress τ_{all} as 18 kpsi. Since τ < τ_{all}, the weld is satisfactory. Since the code already has a design factor of 0.577(50)/18 = 1.6 included at the equality, the corresponding factor of safety to part (a) is

n = 1.6 \frac {18}{8.51} = 3.38

which is consistent.

Table 9–6    Allowable Steady Loads and Minimum Fillet Weld Sizes

Schedule B: Minimum Fillet Weld Size, h Schedule A: Allowable Load for Various Sizes of Fillet Welds

Not to exceed the thickness of the thinner part.
*Minimum size for bridge application does not go below \frac {3}{16} in.
†For minimum fillet weld size, schedule does not go above \frac {3}{16} in fillet weld for every
\frac {3}{4} in material.

Strength Level of Weld Metal (EXX)
60* 110* 100 90* 80 70* 60*
Allowable shear stress on throat, ksi (1000 psi) of fillet weld or partial penetration groove weld
36.0 33.0 30.0 27.0 24.0 21.0 18.0 τ =
llowable Unit Force on Fillet Weld, kip/linear in
25.45h 23.33h 21.21h 19.09h 16.97h 14.85h 12.73h † f =
able Unit Force for Various Sizes of Fillet Welds Leg Size h, in
25.45 23.33 21..21 19.09 16.97 14.85 12.73 1
22.27 20.41 18.57 16.70 14.85 12.99 11.14 7/8
19.09 17.50 15.92 14.32 12.73 11.14 9.55 3/4
15.91 14.58 13.27 11.93 10.61 9.28 7.96 5/8
12.73 11.67 10.61 9.54 8.48 7.42 6.37 1/2
11.14 10.21 9.28 8.35 7.42 6.50 5.57 7/16
9.54 8.75 7.95 7.16 6.36 5.57 4.77 3/8
7.95 7.29 6.63 5.97 5.30 4.64 3.98 5/16
6.36 5.83 5.30 4.77 4.24 3.71 3.18 1/4
4.77 4.38 3.98 3.58 3.18 2.78 2.39 3/16
3.18 2.92 2.65 2.39 2.12 1.86 1.59 1/8
1.59 1.46 1.33 1.19 1.06 0.930 0.795 1/16

*Fillet welds actually tested by the joint AISC-AWS Task Committee.
†f0.707h τ all.

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