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Coupon Test Report

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Coupon test report

LIU, WEI-YI
registration number: 160108260
Date: 03/11/2016

Introduction

The coupon test experiment is set to compare the steel-steel and aluminium-steel plate weld joints regarding their strength and stiffness. The primary values can be obtained through statistical analysis from different groups to avoid sampling errors.

The results can, therefore, be used to decide the strut material and the number of weld points to fit the design specification.

Procedure

The experiment starts with marking welding points on the steel and aluminium rolled tubes as the drawing provided, followed by having them welded on separate sheet metal under the operation of respective spot welders. Each group, then, has their both coupons gripped on the tensometer machine for testing its tensile behaviour. The measured raw data, force over deflection, can be plotted in the graph to find out each coupon’s main characteristics – Maximum Force until failure (Fmax), Limit of Proportionality (Flim), Maximum Deflection before failure (Dmax) and Stiffness. These data collected from each group can, therefore, be clean up and then derived into the final results, Fmax or Flim, in the assumption of normal distribution for the design specification.

Results

As shown in Table 1 and 2, each table contains the group data derived from the testing on Steel coupon and Aluminium coupon. To avoid sampling errors in the final results, statistical analysis is carried out by removing outliers in the data. Therefore, any data outside the range of one standard deviation from the mean value, highlighted in red colour, should be eliminated according to Table 3 and 4. While one of the design specification is no more than 5mm beam displacement under maximum load, the Flim (limit of proportionality) is only the suitable value for both end-fitting designs. The final statistical results of this value for both end-fittings are listed in Table 5.

Group

1

2

3

4

5

6

7

8

9

10

11

12

Max Force, through to failure

Fmax, N

3524

2830

3567

2232

3359

2961

1497

3466

2977

2923

2968

3104

Limit of Proportionality

Flim, N

3068

60

3567

2173

3269

2930

1453

3329

2793

2700

255

2819

Max Deflection, before failure

Dmax, mm

1.00

1.85

4.00

1.06

0.92

1.03

1.53

4.03

2.16

1.23

2.23

2.70

Stiffness in linear region

k, N/mm

2759

300

1327

2743

3158

2790

1646

2879

2655

2822

310

3038

Group

13

14

15

16

17

18

19

20

21

22

23

3455

2328

3456

1225

2.89

0.90

3256

1075

Max Force, through to failure

Fmax, N

1527

3782

2933

2709

3023

2781

2597

2481

3068

3242

2947

Limit of Proportionality

Flim, N

1391

3493

2800

174

2956

2718

2497

509

3042

3010

2832

Max Deflection, before failure

Dmax, mm

1.66

2.60

2.26

3.28

0.80

1.44

0.70

2.80

0.82

2.30

1.15

Stiffness in linear region

k, N/mm

688

2975

2900

107

2778

2707

2875

197

3086

2049

3022

Table 1. Tensile test on Aluminium-steel coupon

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