In the past, experimental investigations as well as theoretical consid
erations have shown that within fronts and inversions wind shear and v
ertical temperature gradient adjust in such a way that the Richardson
number is at its critical value. Results from aircraft measurements no
w suggest that the shear within moving cold fronts, warm fronts and in
versions shows different behaviour because of the different mechanisms
controlling the Richardson numbers. This leads to higher Richardson n
umbers, and therefore to lower amounts of wind shear within moving col
d fronts when compared to warm fronts and inversions.