Abstract
It is well known that the relation between the electron emission i from a hot body and its absolute temperature
T
may be expressed empirically by the equation i =
AT
2
e
-ψ/
kT
, in which
A
and ψ are constants characteristic of the emitting surface, and
k
is Boltzmann’s constant. This is of the same form as the theoretical equation i =
A
0
D
-
T
2
e
-x/
kT
, in which
A
0
is a universal constant having the numerical value of 120 amp. cm.
-2
degree
-2
,
D
-
is the mean transmission coefficient, and
X
is the work function of the emitter. This quantity is not necessarily constant with temperature, and if we assume its temperature variation to be linear, as we may do within a sufficiently restricted range of temperatures, setting
X
= ω+α
KT
, Where ω and α are Constants, we may rewrite(2) thus: i =
A
0
D
-
T
2
e
-ω/
kT
. It may be shown (cf. Reimann 1934a, p. 265) that in such cases as occur in nature
D
-
probably never varies appreciably with temperature, and so, assuming this, and comparing (1) with (4), we may write
A = A
0
D
-
e-α, ψ = ψ
.
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