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Velocity Variation Across a Vertical Cross-Section

The velocities found from the four waves are compared with the theoretical expressions, equations (6.55), (6.56), (6.57) and (6.58), in figures 7-39 - 7-46 where the horizontal

   figure6452
Figure 7-39: The horizontal velocity u as a function of z for wave (1) with tex2html_wrap_inline12323 , tex2html_wrap_inline12193 , tex2html_wrap_inline12453 and f = 1.4 at tex2html_wrap_inline12541 . The solid line is the theoretical curve.

   figure6461
Figure 7-40: The vertical velocity w as a function of z for wave (1) with tex2html_wrap_inline12323 , tex2html_wrap_inline12193 , tex2html_wrap_inline12453 and f = 1.4 at tex2html_wrap_inline12555 . The solid line is the theoretical curve.

   figure6470
Figure 7-41: The horizontal velocity u as a function of z for wave (2) with tex2html_wrap_inline12323 , tex2html_wrap_inline12193 , tex2html_wrap_inline12473 and f = 1.05 at tex2html_wrap_inline12541 . The solid line is the theoretical curve.

   figure6479
Figure 7-42: The vertical velocity w as a function of z for wave (2) with tex2html_wrap_inline12323 , tex2html_wrap_inline12193 , tex2html_wrap_inline12473 and f = 1.05 at tex2html_wrap_inline12583 . The solid line is the theoretical curve.

   figure6488
Figure 7-43: The horizontal velocity u as a function of z for wave (3) with tex2html_wrap_inline12323 , tex2html_wrap_inline12193 , tex2html_wrap_inline12493 and f = 1.86 at tex2html_wrap_inline12541 . The solid line is the theoretical curve.

   figure6497
Figure 7-44: The vertical velocity w as a function of z for wave (3) with tex2html_wrap_inline12323 , tex2html_wrap_inline12193 , tex2html_wrap_inline12493 and f = 1.86 at tex2html_wrap_inline12555 . The solid line is the theoretical curve.

   figure6506
Figure 7-45: The horizontal velocity u as a function of z for wave (4) with tex2html_wrap_inline12323 , tex2html_wrap_inline12511 , tex2html_wrap_inline12453 and f = 1.4 at tex2html_wrap_inline12541 . The solid line is the theoretical curve.

   figure6515
Figure 7-46: The vertical velocity w as a function of z for wave (4) with tex2html_wrap_inline12323 , tex2html_wrap_inline12511 , tex2html_wrap_inline12453 and f = 1.4 at tex2html_wrap_inline12555 . The solid line is the theoretical curve.

velocity is measured at tex2html_wrap_inline12645 , t = T/4 and the vertical velocity at tex2html_wrap_inline12305 , t = T/4. This is where the magnitudes of the velocities are maximum. The solid lines are the theoretical values and the markers are the simulation results. For each wave there is a good agreement for both the magnitude and the shape of the velocity distributions. The poorest fit is for the horizontal velocity in wave (4) where the viscosity is at its largest. Despite the large viscosity tex2html_wrap_inline13299 in equation (6.46) is 0.05 which is still small so the theory should be applicable. The fit is good everywhere except outside the viscous interface region in the upper fluid. At its worst the discrepancy is about tex2html_wrap_inline15237 , about 25%, however the difference is generally much smaller, only a few percent. As predicted in section 6.3.2 the viscosity has little affect on the shape of the vertical velocity distribution, the shape of the graphs in figures 7-40, 7-42, 7-44 and 7-46 all being similar. The difference in the velocity magnitude is due mainly to the different values of tex2html_wrap_inline16851 as would be the case for inviscid waves. The effect of the viscosity is much more evident in the horizontal velocity profiles shown in figures 7-39, 7-41, 7-43 and 7-45. Waves (1) and (3) both show a definite boundary layer, in both fluids, in the region of the solid boundary ( at tex2html_wrap_inline16853 ). The influence of the boundary layer is only obvious within about 10 lattice units of the boundary. Waves (2) and (4) both have very low velocities close to the boundary and there is no noticeable change in the velocity profile. At the interface (z = 0) the effect of the viscosity can be seen readily in each of the waves. The magnitude of the horizontal velocity peaks some distance from the interface and then decreases steadily to zero at the interface. The distance of the peak from the interface is tex2html_wrap_inline16857 lu for waves (1) and (3) and tex2html_wrap_inline14907 lattice units for waves (2) and (4). This is consistent with the values of tex2html_wrap_inline16861 : 7, 15, 5 and 16 given in table 7-1. For waves (1) and (3) tex2html_wrap_inline16861 has a similar value, about a third of the value for waves (2) and (4). Twice this distance from the boundary the magnitude of the irrotational velocity will be reduced a factor of tex2html_wrap_inline16865 to about 14% of its value at the interface/boundary and its effect will become negligible at greater distances.

The results in figures 7-47 and 7-48

     figure6543
Figure 7-48: The vertical velocity w as a function of z for wave (1) at tex2html_wrap_inline12305 and at multiples of T/4.
Figure 7-47: The horizontal velocity u as a function of z for wave (1) at tex2html_wrap_inline12645 and at multiples of T/4.

show the horizontal and the vertical velocity profile respectively at times tex2html_wrap_inline12457 , 3T/4, 5T/4, 7T/4, 9T/4 and 11T/4 for wave (1). The horizontal velocity is shown at tex2html_wrap_inline12645 and the vertical velocity at tex2html_wrap_inline12305 . The decrease in both the horizontal and the vertical velocity with time can be seen over the three periods of oscillation. This is expected at the rate tex2html_wrap_inline15863 since this is the rate at which a, the interface amplitude, is decaying and the velocities are proportional to a. There is also a lack of symmetry about z = 0 which is particularly obvious in the horizontal velocity, see figure 7-47. This is expected since the ratio of the irrotational velocities C1/C2 is 1.4 here.


next up previous contents
Next: Velocity Variation Across a Up: Velocities Previous: Velocities

James Buick
Tue Mar 17 17:29:36 GMT 1998