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Figure 9.1 A laminar boundary layer on a flat plate in a uniform flow. Its thickness
δ(x) is defined as the distance above the surface where the streamwise velocity
reaches a specified fraction of the free-stream velocity U
.
Figure 9.2 An acoustic sounder record from a convective ABL. The ABL is about
200 m deep until 1100 MST, grows to about 400 m at 1230, falls to 200 m at 1330,
and grows to 400 m again at 1400. Photo courtesy W. D. Neff. From Wyngaard
( 1988 ).
The first could be approached when the stress-divergence term is small (as in a deep
convective ABL over a smooth surface, Chapter 11 ) and the mean horizontal momentum
balance (8.65) , in vector form, nears the nonturbulent flow limit
1
ρ 0
0
=−
p
2
×
u .
(9.1)
Since the Coriolis term is perpendicular to u , the dot product of Eq. (9.1) with u is
simply
1
ρ 0
p
·
u
=
0 ,
(9.2)
so that u is parallel to the isobars, as shown in Figure 9.3 . The second bound is approached
in turbulent flow when the Coriolis term is small (as with an inversion at height z i such
 
 
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