Let us substitute this expression into (2.5.35), and then multiply the resulting equations by (cp/f)(T/6)2ya/(ya — y), represent [0] in terms of [7"] and integrate over the whole mass of the atmosphere. Then, finally, we have dA~ = G(AM) - C(AM, KM) - C(AM, AE), (2.5.36)

8t where

G04m) = | S [iv]«2 cos <p dA d<p dp/g, (2.5.38)

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