5 2.5 Bead‐on‐plate welding of a thick‐section carbon steel is carried out using 200 A, 20 V, and 2 mm/s. The preheat temperature and arc efficiency are 100 °C and 60%, respectively. Calculate the cross‐sectional area of the weld bead.
6 2.6 (a) Do you expect to have difficulty in achieving steady‐state heat flow during girth (or circumferential) welding of tubes by keeping constant heat input and welding speed? Explain why. What is the consequence of the difficulty? (b) Suggest two methods that help achieve steady‐state heat flow during girth welding.
7 2.7 A cold‐rolled AISI 1010 low‐carbon steel sheet 0.6 mm thick was tested for surface reflectivity in CO2 laser beam welding under the following different surface conditions: (a) as received; (b) oxidized in air furnace at 1000 °C for 20 s; (c) oxidized in air furnace at 1000°C for 40 s; (d) covered with steel powder. In which order does the reflectivity rank in these surface conditions, and why?
8 2.8 It was observed in yttrium‐aluminum‐garnet (YAG) laser beam welding of AISI 409 stainless steel that under the same power the beam size affected the depth–width ratio of the resultant welds significantly. Describe and explain the effect.
9 2.9 Calculate the peak temperature at the top surface of a very thick carbon steel plate at 5 mm away from the fusion line of the weld surface. The power of the arc is 2 kW, the arc efficiency 0.7, the travel speed 2 mm/s, and the preheat temperature 100 °C.
10 2.10 Compare SAW and ESW. (a) Which one has a higher heat efficiency? (b) Explain why.
11 2.11 Compare GMAW and flux‐cored arc welding (FCAW) under the same power input, travel speed, and filler wire deposition rate. Which weld cool down more slowly, and why?
3 Fluid Flow in Welding
This chapter deals with fluid flow in the arc and the weld pool. It draws heavily on the work at UW‐Madison on computer simulation of weld‐pool convection, flow visualization, weld‐pool surface deformation and oscillation, ripple formation on the weld surface, and how these are affected by the surface‐active agent. The chapter also discusses the recent work on: (i) the metal−vapor effect on fluid flow in the arc, and (ii) fluid flow in the nugget in resistance spot welding (RSW).
3.1 Fluid Flow in Arcs
As shown previously in Figure 2.11, in gas−tungsten arc welding (GTAW) the tip angle of the tungsten electrode has a significant effect on the shape of the arc. The arc tends to become more constricted as the electrode tip changes from sharp to blunt. The change in the shape of the electrode tip changes fluid flow and heat transfer in the arc, which in turn changes the shape of the arc.
3.1.1 Sharp Electrode
Figure 3.1 shows the body‐fitting coordinate system used in the early work of Tsai and Kou [1] on computer simulation of fluid flow and heat transfer in a gas‐tungsten welding arc. Fluid flow and heat transfer in GTAW has been studied by computer simulation [1–6]. An example is the work by Tsai and Kou [1], which demonstrated the significant effect of the electrode tip geometry on the arc. Although the work did not consider the metal vapor in the arc and the pool surface shape as in the more recent work, it is simple and thus useful for explaining basic fluid flow in the arc before discussing more complicated details.
Figure 3.1 Gas‐tungsten welding arc: (a) sketch; (b) body‐fitted grid system for calculation of heat transfer and fluid flow.
Source: Tsai and Kou [1]. © Elsevier.
Figure 3.2 is a schematic sketch of an arc produced by a tungsten electrode with a sharp tip that is truncated. The polarity is DC electrode negative. The electric current converges from the larger workpiece to the smaller electrode tip. It tends to be perpendicular to the electrode tip surface and the workpiece surface (flat), as illustrated in Figure 3.2a. The electric current induces a magnetic field, which is out of the plane of the page (as indicated by the front view of an arrow) on the left and into the page (as indicated by the rear view of an arrow) on the right. The magnetic field and the converging electric‐current field together produce a downward and inward Lorentz force F to push the ionic gas along the conical surface of the electrode tip. The downward momentum is strong enough to cause the high‐temperature ionic gas to impinge on the workpiece surface and turn outward along the workpiece surface, thus producing a bell‐shaped arc, as illustrated in Figure 3.2b.
Figure 3.2 Arc produced by a tungsten electrode with a sharp tip: (a) Lorentz force (F); (b) fluid flow. The directions of Lorentz force and fluid flow shown for DCEN here remain the same for DCEP because the electric current and the magnetic filed it induces are both reversed in direction.
Figure 3.3 (left) shows the current density distribution in a 2 mm long, 200 A arc produced by a 3.2 mm diameter electrode with a 60° angle tip. The electric current near the electrode tip is essentially perpendicular to the surface. The Lorentz force, shown in Figure 3.3 (right), is downward and inward along the conical surface of the electrode tip. As shown in Figure 3.4, this force produces a high velocity jet of more than 200 m/s maximum velocity and the jet is deflected radially outward along the workpiece surface. This deflection of the high‐temperature jet causes the isotherms to push outward along the workpiece surface, thus resulting in a bell‐shaped arc.
Figure 3.3 Current‐density field (left) and Lorentz force (right) in an arc produced by a tungsten electrode with a 60° tip angle.
Source: Tsai and Kou [1]. © Elsevier.
Figure 3.4 Velocity and temperature fields in an arc produced by a tungsten electrode with a 60° tip angle. The isotherms from right to left are 11 000, 13 000, 15 000, 17 000, 19 000, and 21 000 K.
Source: Tsai and Kou [1]. © Elsevier.
3.1.2 Flat‐End Electrode
With a flat‐end electrode, on the other hand, there is no longer a sharp electrode tip