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Publication Number:  FHWA-HRT-17-110    Date:  January 2018
Publication Number: FHWA-HRT-17-110
Date: January 2018

 

Fatigue Performance of High-Frequency Welded Steel I-Beams

SPECIMENS

Six HF-welded, doubly symmetric I-beams consisting of ASTM A769 grade 50 steel were attained to be fatigue tested.(2) The specimens were identified sequentially as beam 1 through beam 6. The nominal geometric properties of the steel I-beams are given in table 1. A picture of a representative partial beam cross section (one flange and most of the web) is shown in figure 1. Most noticeable in this picture is the horizontal offset of the web; while it is joined at the midwidth of the flange, the forging force during welding caused a shift in the web to the left. This distortion of the cross section was observed in all the beams and did cause stability issues that will be described in more depth later. The weld itself, shown in figure 2, appeared very uniform, though the manufacturer of this I-beam did not remove the flash that is ejected from the forging event, and this is noted in the figure and highlighted, as it did affect results described later.

Table 1. Beam specimen nominal geometric properties.

Geometric Property

Nominal
Value

Beam length, L

144 inches

Flange thickness, tf

0.35 inch

Flange width, bf

7.9 inches

Web thickness, tw

0.24 inch

Web height, hw

15.7 inches

Area, A

9.3 inches2

Moment of inertia, I

432.0 inches4

Section modulus, S

55.0 inches3

 

This photo shows a steel, T-shaped cross section. The flange is running horizontally across the bottom of the figure parallel to a ruler. The scale of the ruler is not shown, but the width of the flange is about 8 inches long. The web is vertically oriented and joined at the midwidth of the flange. A straight, dashed vertical line is shown to the left side of the web. The web is parallel to the line except for the lower one unit of length near the joint between the web and flange. It is clear the web suffered a horizontal offset to the left during the welding event.

Source: FHWA.
Note: Scale is in units of inches.

Figure 1. Photo. Beam cross section.

 

This photo shows a macroetch of a small section of web, flange, and the complete joint penetration weld between the two. The flange plate (labeled “Flange”) is oriented horizontally, and the web (labeled “Web”) is vertical. The weld is arc shaped with a low point approximately one-tenth of a web thickness into the flange. A narrow line can be seen through the middle of the weld defining the fusion line, and on each side of the fusion line is a darker heat-affected zone. An irregular-sized piece of metal is shown outside of the joint on each side of the web and is labeled “Flash.” A ruler is provided in the field of view with uniform divisions, though units are not shown. The flange portion is 17 units wide, and by inspection, the web is 8 units high.

Source: FHWA.
Note: Scale is in increments of 1/16 inch.

Figure 2. Photo. Macroetch of weld.

Tension Properties

Tension testing was performed in accordance with ASTM Standard E8 to confirm the steel mechanical properties.( 3 ) Four standard-sized, sheet-type tension specimens were taken from the tension flange of beam 1 after fatigue testing. The samples were taken from a flange near the support that experienced low stresses throughout the fatigue testing period. Strain was monitored with a clip-on extensometer over the 2-inch gauge length of the specimen. Due to software issues while running one of the tests, one specimen was discarded.

Figure 3 shows plots of the tension test results from the three valid specimens tested, and succinct results are presented in table 2. Based on testing averages, the beam specimen steel exhibited a 0.2-percent offset yield strength of 51.6 ksi and an ultimate strength of 71.8 ksi. The fracture location for specimen 2 was very close to one of the extensometer contact points; thus, the elongation percentage at failure for this specimen was not captured accurately by the extensometer readings. This is illustrated by the behavior shown for specimen 2 in the plot of figure 3. The average elongation percentage for the two specimens with valid fracture locations was 42.6 percent, and the average reduction in area was 71.8 percent.

This graph has a horizontal axis labeled “Engineering Strain” ranging from 0.00 on the left to 0.50 on the right in increments of 0.10. The vertical axis is labeled “Engineering Stress (in units of ksi)” ranging from 0 on the bottom to 80 at the top in increments of 20. Three plots are shown in the plot labeled “1,” “2,” and “4” at the point of fracture. All three plots show linear elastic behavior up to approximately 50 ksi, and then each begins to round over into strain hardening behavior. Plots 1 and 4 show similar behavior peaking at approximately 70 ksi of stress and 0.23 strain; then stress begins to decrease, and 1 fractures at a strain of approximately 0.40, and 4 fractures at a strain of 0.45. Plot 2 strain hardened to a stress plateau of about 73 ksi at a strain of 0.20 and fractured shortly thereafter at a strain of 0.25.

Source: FHWA.

Figure 3. Graph. Tension test results.

 

Table 2. Results of tensile tests.

Specimen

0.2 Percent Offset Yield
(ksi)

Tensile Strength
(ksi)

Extensometer Elongation
(percent)

Reduction in Area
(percent)

1

52.7

70.7

40.3

71.8

2

51.1

73.3

25.9

61.4

4

51.1

71.5

45.0

71.8

 

 

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