- Open Access
- Total Downloads : 278
- Authors : Ravindra B. Kulkarni, Vishal Vaghe
- Paper ID : IJERTV2IS2603
- Volume & Issue : Volume 02, Issue 02 (February 2013)
- Published (First Online): 28-02-2013
- ISSN (Online) : 2278-0181
- Publisher Name : IJERT
- License: This work is licensed under a Creative Commons Attribution 4.0 International License
Experimental Study of Bolted Connections Using Light Gauge Channel Sections, Using Stiffener/Packing Plates at the Joints
Ravindra B. Kulkarni* and Vishal Vaghe**
*Asst. Professor, ** M-Tech. Student.
Department of Civil Engineering
Gogte Institute of Technology, Belgaum 590008 (Karnataka)
Abstract
Cold-formed structural members are being used more widely in routine structural design as the world steel industry moves from the production of hot-rolled section and plate to coil and strip, often with galvanised and/or painted coatings. Steel in this form is more easily delivered from the steel mill to the manufacturing plant where it is usually cold-rolled into open and closed section members. The present study is focus on examining the experimental investigation to study the effect of Stiffener/Packing plate (Mild steel Plates) only at the joints in cold formed channel sections by using bolts at the joints and which may increase the load carrying capacity of the bolted channel section subjected to axial tension. In the present study, the strength of the joint is increased by increasing the various thicknesses of Stiffener/Packing plates at the joints with three numbers of bolts at the connection. And also the experiment is executed with a single bolt to study the of failure pattern at the joints. Total Twelve experimental tests have been carried out on cold formed channel tension members fastened with bolts, to calculate the failure capacity and increase in strength of the member and also to trace the entire load versus elongation path, so that the behavior of the connection is examined.
Keywords: Light Gauge Steel Sections, Steel Plates, Strain/Elongation, Failure Patterns.
Introduction
The use of cold-formed steel members in building construction began in the 1850s in both the United States and Great Britain. In the 1920s and 1930s, acceptance of cold-formed steel as a construction material was still limited because there was no adequate design standard and limited information on material use in building codes. One of the first documented uses of cold-formed steel as a building material is the Virginia Baptist Hospital, constructed around 1925 in Lynchburg, Virginia. The walls were load bearing masonry, but the floor system was framed with double back-to-back cold- formed steel lipped channels. According to
Chuck Greene, P.E of Nolen Frisa Associates [2], the joists were adequate to carry the initial loads and spans, based on current analysis techniques. Greece engineered a recent renovation to the structure and said that for the most part, the joists are still performing well. A site observation during this renovation confirmed that "these joists from the 'roaring twenties' are still supporting loads, over 80 years later!" In the 1940s, Lustron Homes built and sold almost 2500 steel-framed homes, with the framing, finishes, cabinets and furniture made from cold-formed steel.[1]
Cold-Formed Steel (CFS) is the common term for products made by rolling or pressing thin gauges of sheet steel into goods. Cold-formed steel goods are created by the working of sheet steel using stamping, rolling, or presses to deform the sheet into a usable product. The use of cold- formed steel construction materials has become more and more popular since its initial introduction of codified standards in 1946. In the construction industry both structural and non-structural elements are created from thin gauges of sheet steel. The material thicknesses for such thin-walled steel members usually range from 0.0147 in. (0.373 mm) to about ¼ in. (6.35 mm). Steel plates and bars as thick as 1 in. (25.4 mm) can also be cold-formed successfully into structural shapes. These building materials encompass columns, beams, joists, studs, floor decking, built-up sections and other components. The manufacturing of cold- formed steel products occurs at room temperature using rolling or pressing. The strength of elements used for design is usually governed by buckling. [2]
Tension Member
Tension members are structural elements or members that are subjected to axial tensile forces. Fig.1 shows a member under tension. They are usually used in different types of structures. Examples of tension members are: bracing for buildings and bridges, truss members and cables in suspended roof systems.
Figure 1: Member under Tension
Stress is given by, F =P/A
Where, P is the magnitude of the load
A is the cross-sectional area
The increase in the length of a member due to axial tension under service load is
=PL / (E.Ag)
Where,
is the axial elongation of the member (mm),P is the axial tensile force (un- factored) in the member (N),L is the length of the member (mm) and E is the modulus of elasticity of steel=2.0×105 MPa.
Note: That displacement is a serviceability limit state criterion and hence is checked
Material Details
Fig 2: Cross section details of channal section
Where,
400.00
350.00
400.00
350.00
Sample
1.5mm Thick Cold Form Plate
Sample
1.5mm Thick Cold Form Plate
300.00
250.00
200.00
150.00
100.00
50.00
300.00
250.00
200.00
150.00
100.00
50.00
h – is the height of the section b – is the width of the section
Stress N/mm2
Stress N/mm2
t – is the thickness of the section r – is the radius section
Ixx and Iyy is the moment of inertia about x and y axis
1.5mm thick plate
1.5mm thick plate
Yield Strength and Youngs Modulus of the Cold Form Channel Specimen
The parallel length is kept between Lo + b/2 & Lo + 2b
Fig 3: Tensile Test on Cold Formed steel Sheet
0.00
0.00
Strian
Strian
0.0000
0.0119
0.0238
0.0358
0.0477
0.0596
0.0715
0.0835
0.0954
0.1073
0.1192
0.1312
0.1431
0.1531
0.1574
0.1693
0.1812
0.1932
0.0000
0.0119
0.0238
0.0358
0.0477
0.0596
0.0715
0.0835
0.0954
0.1073
0.1192
0.1312
0.1431
0.1531
0.1574
0.1693
0.1812
0.1932
Fig 5: Graph Between Force and Elongation for 1.5mmThick Cold form plate
Test Samples |
Thickness of sample |
Yield Stress |
ultimate strength |
Young's Modulus |
No |
mm |
N/mm2 |
N/mm2 |
KN/mm2 |
1 |
1.2 |
231.67 |
358.33 |
191.81 |
2 |
1.5 |
233.55 |
357.77 |
207.57 |
Test Samples |
Thickness of sample |
Yield Stress |
ultimate strength |
Young's Modulus |
No |
mm |
N/mm2 |
N/mm2 |
KN/mm2 |
1 |
1.2 |
231.67 |
358.33 |
191.81 |
2 |
1.5 |
233.55 |
357.77 |
207.57 |
Table -1: Yield Strength and Youngs Modulus Cold form steel plate
Where,
400.00
350.00
Stress N/mm2
Stress N/mm2
300.00
p>250.00
200.00
150.00
100.00
50.00
0.00
Lo = Original Gauge length Le = Parallel length
Lt = Total length
b = Width of the test piece
Sample 1
1.2mm Thick Cold Form Plate
0.0000
0.0164
0.0328
0.0492
0.0655
0.0819
0.0983
0.1147
0.1311
0.1475
0.1638
0.1759
0.1884
0.2048
0.2212
0.0000
0.0164
0.0328
0.0492
0.0655
0.0819
0.0983
0.1147
0.1311
0.1475
0.1638
0.1759
0.1884
0.2048
0.2212
1.2mm thick plate
Stain
Hence from the IS 1079-1973 the Grade of the steel is referred to as St.42 for the yield stress 235 N/mm2
Materials used as Stiffener/Packing Plate (Mild Steel Plate) at the Joint
-
A high amount of carbon makes mild steel different from other types of steel. Carbon makes mild steel stronger and stiffer than other type of steel. However, the hardness comes at the price of a decrease in the ductility of this alloy. Carbon atoms get affixed in the interstitial sites of the iron lattice and make it stronger.
-
Mildest grade of carbon steel or 'mild
Fig 4: Graph Between Force and Elongation for 1.2mmThick Cold form plate
steel' is typically carbon steel, with a
comparatively mild amount of carbon (0.16% to 0.19%).
-
The calculated average industry grade mild steel density is 7.85 gm/cm3. Its Young's modulus, which is a measure of its stiffness, is around 210,000 Mpa.
-
Mild steel is the cheapest and most versatile form of steel and serves every application which requires a bulk amount of steel.
Connections
Connections designed more conservatively than members because they are more complex to analyse and discrepancy between analysis and design is large. Connections are normally made either by bolting or welding. Bolting is common in field connections, since it is simple and economical to make. Bolting is also regarded as being more appropriate in field connections from considerations of safety.
Types of Failure Mode in Connections
-
Longitudinal shear failure of sheet (type I).
-
Bearing failure f sheet (type II). (c)Tensile failure of sheet (type III)
(d) Shear failure of bolt (type IV).
Fig 6: Types of failure of bolted connections
Experimental Tests Specimens Geometries
The experimental testing consists of
channel of tension specimens fabricated from rolled steel sheets. All specimens are of 500 mm length. All specimens are fastened, with a single row of 12 mm diameter HSFG GR 8.8 bolts, through their webs at both ends. The tests consist of 3 sets of channel of size 50x40mm specimens with the 1.2 and 1.5mm thickness, with the same connection length for all the samples. At the connection Stiffener/Packing plates are used of different thickness. The end distance and number of bolts for each specimen are held constant at 24 mm and 3 numbers respectively, with Holes for the 12mm GR
-
bolts were specified to be drilled to a 14 mm diameter.
Table-2 Specimen Dimensions for 1.2mm Thick Channel with 3 Bolts Connection
Specime n Size
No of Bolts
End Dist
Connecting Length
Thickness of plate
Dia of Bolt
Dia of Hole
50X40
3
24
72
1.2
12
14
50X40
3
24
72
1.2
12
14
50X40
3
24
72
1.2
12
14
50X40
3
24
72
1.2
12
14
50X40
3
24
72
1.2
12
14
(All dimensions are in mm)
Table-3 Specimen Dimensions for 1.5mm Thick Channel with 3 Bolts Connection
Specimen Size
No of Bolts
End Dist
Connecting Length
Thickness of plate
Dia of Bolt
Dia of Hole
50X40
3
24
72
1.5
12
14
50X40
3
24
72
1.5
12
14
50X40
3
24
72
1.5
12
14
50X40
3
24
72
1.5
12
14
50X40
3
24
72
1.5
12
14
(All dimensions are in mm)
Table-4 Specimen Dimensions for 1.5mm Thick Channel with single Bolts Connection at the joint
Specimen No
No of Bolts
End Dist
Connecting Length
Thickness of plate
Dia of Bolt
Dia of Hole
50X40
3
24
72
1.5
12
14
50X40
3
24
72
1.5
12
14
(All dimensions are in mm)
Set up of Channel section moulds, are used to transfer the load from a 1000 KN universal testing machine (UTM) to a Channel specimen.
Fig 7: Channel moulds for the proper grip used for connecting channel section to UTM for Tensile test
-
Sample without b) Sample with
-
Packing plate packing plate Fig 8: Specimen Geometries of the test sample with
3 bolts connection at the bottom
a) Sample without b) Sample with
Packing plate packing plate Fig 9: Specimen Geometries of the test sample with
single bolts connection at the bottom
Experimental Procedures and Results
Twelve full-scale bolted connections were tested in tension in a 1000 kN (tension) capacity universal testing machine. The load was applied quasi-statically. Readings of load and displacement were taken at regular intervals 12mm diameter HYSD Bolts were used, diameter hole of 14mm was drilled in both the 5mm thick plate as shown in the figure: 8. three such bolts were used to fasten these two plates together. These bolts were tightened using the turn of the nut method.
Fig 10: Arrangement made for tensile testing for UTM
Test Descriptions and Results
A summary of the test results and description of each test is presented in the following sections.
Specimens of Series A (1.2 mm Thick Channel Specimen with Three Numbers of Bolts at the Joint) Specimens of Series B (1.5 mm Thick Channel Specimen with Three Numbers of Bolts at the Joint)
In this five specimens are used having the same cross section and the only variable was the thickness of the Stiffener/Packing Plate, which was 2mm, 3mm, 4mm, and 5mm. and first sample is tested without Stiffener/ packing plate. The results will be plotted to Load vs. deformation curves for these five specimens.
Specimens of Series C (1.5mm Thick Channel Specimen with Single Number of Bolt at the Joint)
In this two specimens are used having the same cross section and the thickness of the Stiffener/Packing Plate used was 4mm, and first sample is tested without Stiffener/packing plate. The results will be plotted to Load vs. deformation curves for these five specimens.
Results
Specimens of Series A (1.2 mm Thick Channel Specimen with Three Numbers of Bolts at the Joint)
Sample -1
350.00 |
|||
250.00 |
300.00 |
||
200.00 150.00 100.00 50.00 0.00 |
Without stiffener plate Strain |
250.00 200.00 150.00 100.00 50.00 0.00 |
350.00 |
|||
250.00 |
300.00 |
||
200.00 150.00 100.00 50.00 0.00 |
Without stiffener plate Strain |
250.00 200.00 150.00 100.00 50.00 0.00 |
300.00 50x40x1.2 without stiffner plate
Sample -4
50x40x1.2 with 4mm stiffner plate
Stress N/mm2
Stress N/mm2
0.0000
0.0055
0.0110
0.0165
0.0220
0.0275
0.0330
0.0385
0.0440
0.0495
0.0550
0.0605
0.0660
0.0715
0.0770
0.0825
0.0000
0.0055
0.0110
0.0165
0.0220
0.0275
0.0330
0.0385
0.0440
0.0495
0.0550
0.0605
0.0660
0.0715
0.0770
0.0825
Stress N/mm2
Stress N/mm2
0.0000
0.0090
0.0180
0.0270
0.0360
0.0450
0.0540
0.0630
0.0720
0.0810
0.0900
0.0968
0.1058
0.1148
0.1220
0.0000
0.0090
0.0180
0.0270
0.0360
0.0450
0.0540
0.0630
0.0720
0.0810
0.0900
0.0968
0.1058
0.1148
0.1220
Without stiffener plate 4mm thick Stiffener Plate
Fig 11: Graph between stress and strain for SMPL-1 without Stiffener/Packing plate
Strain
Fig 14: Comparison Graph between stress and strain for SMPL-4 with 4mm thick Stiffener/Packing plate
300.00
250.00
Stress N/mm2
Stress N/mm2
200.00
Sample -2
350.00
350.00
Sample -5
50x40x1.2 with 5mm stiffner plate
Sample -5
50x40x1.2 with 5mm stiffner plate
50x40x1.2 with 2mm stiffner plate
300.00
250.00
200.00
150.00
100.00
50.00
300.00
250.00
200.00
150.00
100.00
50.00
Stress N/mm2
Stress N/mm2
150.00
100.00
without stiffner plate 5mm thick Stiffener Plate
without stiffner plate 5mm thick Stiffener Plate
50.00 Without stiffener plate
with 2mm stiffner plate
0.00
0.00
0.0000
0.0063
0.0125
0.0188
0.0250
0.0313
0.0375
0.0437
0.0500
0.0562
0.0625
0.0687
0.0725
0.0737
0.0792
0.0854
0.0917
0.0979
0.1042
0.0000
0.0063
0.0125
0.0188
0.0250
0.0313
0.0375
0.0437
0.0500
0.0562
0.0625
0.0687
0.0725
0.0737
0.0792
0.0854
0.0917
0.0979
0.1042
0.0000
0.0070
0.0140
0.0210
0.0280
0.0350
0.0420
0.0490
0.0560
0.0630
0.0700
0.0770
0.0840
0.0910
0.0980
0.1031
0.1097
0.1167
0.1237
0.1288
0.0000
0.0070
0.0140
0.0210
0.0280
0.0350
0.0420
0.0490
0.0560
0.0630
0.0700
0.0770
0.0840
0.0910
0.0980
0.1031
0.1097
0.1167
0.1237
0.1288
0.00
Strain
Fig 12: Comparison Graph between stress and strain for SMPL-2 with 2mm thick Stiffener/Packing plate
Strain
Strain
Fig 15: Comparison Graph between stress and strain for SMPL-5 with 5mm thick Stiffener/Packing plate
Sample -3
50x40x1.2 with 3mm stiffner plate
300.00
All Five 1.2 mm Thick channel Samples
50.00 No Packing Plate
45.00
45.00
with 2mm thick stiffener plate with 3mm thick stiffener plate
250.00
Stress N/mm2
Stress N/mm2
200.00
150.00
100.00
50.00 without stiffener plate
40.00
35.00
Force kN
Force kN
30.00
25.00
20.00
15.00
10.00
with 4mm thick stiffener plate with 5mm thick stiffener plate
3mm thick Stiffener Plate
0.0000
0.0065
0.0130
0.0195
0.0260
0.0325
0.0390
0.0455
0.0520
0.0585
0.0650
0.0715
0.0780
0.0845
0.0893
0.0953
0.1018
0.1083
0.1148
0.0000
0.0065
0.0130
0.0195
0.0260
0.0325
0.0390
0.0455
0.0520
0.0585
0.0650
0.0715
0.0780
0.0845
0.0893
0.0953
0.1018
0.1083
0.1148
0.00
5.00
0.00
3.00
6.00
9.00
12.00
15.00
18.00
21.00
24.00
27.00
30.00
33.00
36.00
39.00
42.00
44.20
47.00
50.00
53.00
55.20
0.00
3.00
6.00
9.00
12.00
15.00
18.00
21.00
24.00
27.00
30.00
33.00
36.00
39.00
42.00
44.20
47.00
50.00
53.00
55.20
0.00
Strain
Fig 13: Comparison Graph between stress and strain for SMPL-3 with 3mm thick Stiffener/Packing plate
Elongation
Fig 16: Comparison Graph between Force and Elongation for all the five samples
54.00
Increase in the Ultimate Tensile Strength
300.00
Sample -2
50x40x1.5 with 2mm stiffner plate
54.00
Increase in the Ultimate Tensile Strength
300.00
Sample -2
50x40x1.5 with 2mm stiffner plate
Thickness of Packing plate mm
Strain
Thickness of Packing plate mm
Strain
53.00
52.00
51.00
50.00
49.00
53.00
52.00
51.00
50.00
49.00
Ultimate strength
Ultimate strength
48.00
47.00
48.00
47.00
0
0
2
2
3
3
4
4
5
5
250.00
200.00
150.00
100.00
50.00
250.00
200.00
150.00
100.00
50.00
without stiffener plate with 2mm stiffener plate
without stiffener plate with 2mm stiffener plate
0.00
0.00
Force kN
Force kN
Stress
Stress
N/mm2
N/mm2
0.0000
0.0075
0.0150
0.0225
0.0300
0.0375
0.0450
0.0525
0.0600
0.0675
0.0750
0.0825
0.0900
0.0975
0.1050
0.1080
0.1150
0.1225
0.1300
0.1370
0.0000
0.0075
0.0150
0.0225
0.0300
0.0375
0.0450
0.0525
0.0600
0.0675
0.0750
0.0825
0.0900
0.0975
0.1050
0.1080
0.1150
0.1225
0.1300
0.1370
Fig 17: Graph between Thicknesses of the Stiffener/Packing Plate to ultimate Strength
Fig 19: Comparison Graph between stress and strain for SMPL-2 with 2mm thick Stiffener/Packing plate
Table-5 Results of All the 1.2mm Thick Channel Specimen
300.00
Sample -3
50x40x1.5 with 3mm stiffner plate
N/mm2
N/mm2
Thickness |
%of |
||||||
Specimen Net Section |
Ultimate Tensile |
of Stiffener |
Elongatio n at Peak |
increas |
250.00 |
||
No Area |
Strength |
/Packing |
Load |
strengt |
200.00 |
||
plate |
h |
||||||
mm2 |
kN |
mm |
mm |
% |
150.00 |
||
SMPL-1 136.32 |
34.16 |
– |
31.00 |
0.00 |
100.00 |
||
SMPL-2 |
136.32 |
35.90 |
2 |
35.40 |
4.60 |
50.00 |
|
SMPL-3 |
136.32 |
37.50 |
3 |
40.80 |
7.15 |
0.00 |
|
SMPL-4 |
136.32 |
40.90 |
4 |
41.20 |
19.60 |
||
SMPL-5 |
136.32 |
43.50 |
5 |
43.80 |
26.90 |
Strain |
Thickness |
%of |
||||||
Specimen Net Section |
Ultimate Tensile |
of Stiffener |
Elongatio n at Peak |
increas |
250.00 |
||
No Area |
Strength |
/Packing |
Load |
strengt |
200.00 |
||
plate |
h |
||||||
mm2 |
kN |
mm |
mm |
% |
150.00 |
||
SMPL-1 136.32 |
34.16 |
– |
31.00 |
0.00 |
100.00 |
||
SMPL-2 |
136.32 |
35.90 |
2 |
35.40 |
4.60 |
50.00 |
|
SMPL-3 |
136.32 |
37.50 |
3 |
40.80 |
7.15 |
0.00 |
|
SMPL-4 |
136.32 |
40.90 |
4 |
41.20 |
19.60 |
||
SMPL-5 |
136.32 |
43.50 |
5 |
43.80 |
26.90 |
Strain |
e in
Stress
Stress
0.0000
0.0123
0.0247
0.0370
0.0493
0.0617
0.0740
0.0863
0.0987
0.1110
0.1233
0.1357
0.1394
0.1480
0.1603
0.1727
0.1850
0.0000
0.0123
0.0247
0.0370
0.0493
0.0617
0.0740
0.0863
0.0987
0.1110
0.1233
0.1357
0.1394
0.1480
0.1603
0.1727
0.1850
without stiffener plate with 3mm stiffener plate
Specimens of Series B (1.5 mm Thick Channel Specimen with Three Numbers of Bolts at the Joint)
Fig 20: Comparison Graph between stress and strain for SMPL-3 with 3mm thick Stiffener/Packing plate
Sample -4
Sample -1
50x40x1.5 without stiffner plate
Sample -1
50x40x1.5 without stiffner plate
350.00
300.00
300.00
250.00
200.00
150.00
100.00
50.00
250.00
200.00
150.00
100.00
50.00
300.00
N/mm2
N/mm2
N/mm2
N/mm2
250.00
200.00
Stress
Stress
Stress
Stress
150.00
100.00
50.00
without stiffener plate
without stiffener plate
0.00
0.00
0.0000
0.0060
0.0120
0.0180
0.0240
0.0300
0.0360
0.0420
0.0480
0.0540
0.0600
0.0660
0.0720
0.0780
0.0836
0.0848
0.0860
0.0920
0.0980
0.1040
0.0000
0.0060
0.0120
0.0180
0.0240
0.0300
0.0360
0.0420
0.0480
0.0540
0.0600
0.0660
0.0720
0.0780
0.0836
0.0848
0.0860
0.0920
0.0980
0.1040
0.00
50x40x1.5 with 4mm stiffener plate
0.0000
0.0077
0.0153
0.0230
0.0307
0.0383
0.0460
0.0537
0.0613
0.0690
0.0767
0.0843
0.0920
0.0935
0.0997
0.1073
0.1150
0.0000
0.0077
0.0153
0.0230
0.0307
0.0383
0.0460
0.0537
0.0613
0.0690
0.0767
0.0843
0.0920
0.0935
0.0997
0.1073
0.1150
without stiffener plate with 4mm stiffener plate
Strain
Strain
Fig 18: Graph between stress and strain for SMPL-1 without Stiffener/Packing plate
Strain
Fig 21: Comparison Graph between stress and strain for SMPL-2 with 2mm thick Stiffener/Packing plate
Sample -5
50x40x1.5 with 5mm stiffener plate
350.00
300.00
250.00
200.00
150.00
100.00
50.00 without stiffener plate
with 5mm stiffener plate
0.00
Strain
Sample -5
50x40x1.5 with 5mm stiffener plate
350.00
300.00
250.00
200.00
150.00
100.00
50.00 without stiffener plate
with 5mm stiffener plate
0.00
Strain
Stress
Stress
N/mm2
N/mm2
0.0000
0.0073
0.0147
0.0220
0.0293
0.0367
0.0440
0.0513
0.0587
0.0660
0.0733
0.0807
0.0880
0.0953
0.1027
0.1100
0.1173
0.0000
0.0073
0.0147
0.0220
0.0293
0.0367
0.0440
0.0513
0.0587
0.0660
0.0733
0.0807
0.0880
0.0953
0.1027
0.1100
0.1173
Fig 22: Comparison Graph between stress and strain for SMPL-2 with 2mm thick Stiffener/Packing plate
All Five 1.5 mm Thick channel Samples
without stiffener plate
400.00 With 2mm stiffener plate
350.00 |
with 4mm stiffener plate With 5mm stiffner plate |
80.00 |
300.00 |
70.00 |
|
250.00 |
60.00 |
|
200.00 150.00 100.00 50.00 0.00 Fig 23 |
Strain : Comparison Graph between Force and |
50.00 40.00 30.00 20.00 10.00 0.00 |
350.00 |
with 4mm stiffener plate With 5mm stiffner plate |
80.00 |
300.00 |
70.00 |
|
250.00 |
60.00 |
|
200.00 150.00 100.00 50.00 0.00 Fig 23 |
Strain : Comparison Graph between Force and |
50.00 40.00 30.00 20.00 10.00 0.00 |
with 3mm stiffener plate
Table-6 Results of All the 1.2mm Thick Channel Specimen
Specimen No |
Net Section Area |
Ultimate Tensile Strength |
Thickness of Stiffener /Packing plate |
Elongation at Peak Load |
%of increase in strength |
mm2 |
kN |
mm |
mm |
% |
|
SMPL-1 |
169.5 |
42.40 |
– |
42.80 |
0.00 |
SMPL-2 |
169.5 |
44.90 |
2 |
43.20 |
4.90 |
SMPL-3 |
169.5 |
46.90 |
3 |
45.40 |
9.50 |
SMPL-4 |
169.5 |
48.80 |
4 |
48.80 |
14.0 |
SMPL-5 |
169.5 |
50.40 |
5 |
53.60 |
20.00 |
Specimens of Series C (1.5 mm Thick Channel Specimen with single Bolt at the Joint)
Sample -A
Stress N/mm2
Stress N/mm2
N/mm2
N/mm2
50x40x1.5 without stiffner plate
0.00
3.40
6.80
10.20
13.60
17.00
20.40
23.80
27.20
30.60
34.00
37.40
40.80
44.20
47.60
51.00
54.40
57.80
61.20
64.60
0.00
3.40
6.80
10.20
13.60
17.00
20.40
23.80
27.20
30.60
34.00
37.40
40.80
44.20
47.60
51.00
54.40
57.80
61.20
64.60
Stress
Stress
0.0000
0.0096
0.0192
0.0288
0.0383
0.0479
0.0575
0.0671
0.0767
0.0862
0.0958
0.1054
0.1150
0.1246
0.1342
0.1438
0.0000
0.0096
0.0192
0.0288
0.0383
0.0479
0.0575
0.0671
0.0767
0.0862
0.0958
0.1054
0.1150
0.1246
0.1342
0.1438
Sample -A
Elongation for all the five samples
Increase in Ultimate Tensile strength
52.00
Strain
Fig 25: Graph 6.46: Between Force and Elongation for specimen SMPL-A without Packing plate
Sample -A & B
50.00
Force kN
Force kN
48.00
46.00
44.00
42.00
40.00
Ultimate strength
120.00
100.00
N/mm2
N/mm2
80.00
Stress
Stress
60.00
40.00
50x40x1.5 with 4mm stiffner plate
38.00
0 2 3 4 5
Thickness of Packing Plate mm
20.00 Sample -A
4mm stiffner
0.0000
0.0124
0.0249
0.0373
0.0497
0.0621
0.0746
0.0870
0.0994
0.1119
0.1243
0.1367
0.1491
0.1616
0.1740
0.1864
0.0000
0.0124
0.0249
0.0373
0.0497
0.0621
0.0746
0.0870
0.0994
0.1119
0.1243
0.1367
0.1491
0.1616
0.1740
0.1864
0.00
Fig 24: Graph between Thicknesses of the Stiffener/Packing Plate to ultimate Strength
Strain
Fig 26: Graph 6.46: Between Force and Elongation for specimen SMPL-B with 4mm packing plate
Table-7 Results of 1.5mm Thick Channel section with single bolt at joint
Specimen No |
Net Section Area |
Ultimate Tensile Strength |
Thickness of Stiffener /Packing plate |
Elongation at Peak Load |
% of increase in strength |
mm2 |
kN |
mm |
mm |
% |
|
SMPL-1 |
136.32 |
12.85 |
– |
24.00 |
0.00 |
SMPL-2 |
136.32 |
17.40 |
4 |
28.00 |
35.40 |
20.00
18.00
Utlimate Force kN
Utlimate Force kN
16.00
14.00
12.00
10.00
8.00
6.00
4.00
2.00
0.00
Increase in Ultimate strength
Ultimate strength
0 4
Thickness of stiffner plate
Bearing + Rupture Failure Observed With 2mm Thick Packing Plate for 1.2, and 1.5mm thick specimen sample
Fig 27: Graph between Thicknesses of the Stiffener/Packing Plate to ultimate Strength
Failure Patterns
Bearing + Rupture Failure Observed
Bearing + Rupture Failure Observed With 3mm Thick Packing Plate for 1.2, and 1.5mm thick specimen sample
Vertical Shear Failure of 1.5mm Thick Sample Specimen using 4mm thick Stiffener/packing plate
Block Shear Failure of 1.5mm Thick Sample Specimen using 5mm thick Stiffener/packing plate
Buckling of Stiffener/Packing plate used 1.5mm Thick Sample Specimen
Bearing + Shear Failure Observed for 1.5mm thick specimen sample with single bolted connection
Discussions and Conclusions
Table-8 Results of 1.2mm Thick Channel section with 3 bolts at the Joints
Size of the Specimen |
Thickness of Stiffener /Packing Plate |
Ultimate Tensile Strength |
% of increase in Strength |
Types of Failure observed |
mm |
mm |
(kN) |
% |
|
50X40X1.2 |
– |
34.16 |
0.00 |
Bearing + Rupture |
50X40X1.2 |
2 |
35.90 |
4.60 |
Bearing + Rupture |
50X40X1.2 |
3 |
37.50 |
7.15 |
Bearing + Rupture |
50X40X1.2 |
4 |
40.90 |
19.6 |
Bearing + Rupture |
50X40X1.2 |
5 |
43.50 |
26.9 |
Bearing + Rupture |
Table-9 Results of 1.5mm Thick Channel section with 3 bolts at the Joints
Size of the Specimen |
Thickness of Stiffener /Packing Plate |
Ultimate Tensile Strength |
% of increase in Strength |
Types of Failure observed |
mm |
mm |
(kN) |
% |
|
50X40X1.5 |
– |
42.40 |
0.00 |
Bearing + Rupture |
50X40X1.5 |
2 |
44.90 |
4.90 |
Bearing + Rupture |
50X40X1.5 |
3 |
46.90 |
9.50 |
Bearing + Rupture |
50X40X1.5 |
4 |
48.80 |
14.00 |
Vertical shear |
50X40X1.5 |
5 |
50.40 |
20.00 |
Block shear Failure |
Table-10 Results of 1.5mm Thick Channel section with single bolt at joint
Size of the Specimen |
Thickness of Stiffener /Packing Plate |
Ultimate Tensile Strength |
% of increase in Strength |
Types of Failure observed |
mm |
mm |
(kN) |
% |
|
50X40X1.5 |
– |
12.85 |
0.00 |
Bearing + Shear |
50X40X1.5 |
4 |
17.40 |
35.40 |
Bearing + Shear |
-
It is observed from the above Tables by the use of packing plates the load carrying capacity of the joint increases. As the thickness of the light gauge section increases the variation in increase of joint strength reduces for
various thicknesses of Stiffener/packing plates.
-
For 1.2mm thick channel section it is observed that all failures are due to rupture with 3 bolts connection, and also for 1.5mm thick channel section up to 3mm thick Stiffener/Packing plate failure are due to rupture and for 4mm thick Stiffener/packing plate the failure is due to vertical shear failure along the line of vertical connection. With use of 5 mm thick Stiffener/packing plates the failure is due to block shear failure.
-
Hence with the use of thicker plates, bearing failure can be avoided. The increase in the tensile strength for change in each thickness of the Stiffener/packing plate is shown in Table 8 and 9.
-
By the use of lesser thickness of the Packing plate it is observed that the plate buckles along with the plate.
-
For 1.5mm thick channel section with single bolt at 3d end distance, it is observed that the failure is due to bearing and shear failure and the percentage of increase in tensile strength with 4mm thick Stiffener/packing plate is 35.40%.
References
-
Ed.Chaen Wai-Yu, W.W.Cold formed steel Structures Structural engineering Hand Book.
-
By, Xiao-Ling Zhao Tim Wilkinson and Gregory Hancock Cold Formed Tubular Members And Connections January 2005.
-
Experimental Studies on Cold-Formed Steel Angle Tension Members By
Prabha P, Saravananm, Marimuthu V, and Arulayachandran.
-
Testing of bolted cold formed steel connections in bearing (with and without washers) By James A. Wallace.
-
ColdFormed Steel Frame with
Bolted Moment Connections By, Bayan Anwer Ali, Sariffuddin Saad, Mo hd Hanim.
-
Cyclic Testing of Cold-Formed Steel Special Bolted Moment Frame Connections By Jong-Kook Hong, Atsushi Sato, Chia-Ming Uang, and Ken Wood.
-
Riveted and bolted jointsBy Munse and Chesson [1] in 1963.
-
Shear lag in bolted angle tension members By Kulak and Wu [7] in 1997.
-
Pan [11] in 2004 studied the prediction of the strength of bolted cold-formed channel sections in tension.
-
Barth et al. [9] in 2002 studied Behavior of steel tension members subjected to uniaxial loading.
-
Bouchair et al. [16] In 2008 studied Analysis of the behavior of stainless steel bolted connections.
-
Failure Modes of Bolted Sheet Steel By Colin A Rogers, Gregory J Hancock.
-
Bolted connections by Prof. S.R.Satish Kumar and Prof. A.R.Santha Kumar.
-
Failure mode of steel in tension member due to change in connection eccentricity and connection length by Diwakar Kumar.