2 Resurrection of the Bohr/Sommerfeld Theory of Atomic
Structure.
2.1 Quantum Number Nomenclature.
The current nomenclature for quantum numbers in atomic structure theory is
not used in this paper. A new one, (similar to that of Sommerfeld), is used
for two reasons. Firstly, it introduces a degree of rationalisation and
secondly, the list differs slightly from those currently used. The table
below provides a comparative list.
| Name | Current Nomenclature
| Value | New | Value |
| Principle | n | 1 to ¥ | n | 1 to ¥ |
| Azimuthal | k | 1 to n | nf | 1 to n |
| Orbital | l | 0 to (n-1) | Not Used | - |
| Radial | n/ | n-k | nr | n - nf |
| Spin | s | s1 = + 1/ 2
s2 = - 1/ 2 | nsp | ± 1/ 2 |
| Inner | j | 1/ 2 for l = 0 l+s for l ¹ 0 | nj | nf+nsp |
Table 2.1 - Quantum Number Nomenclature.
Where relativistic effects are to be included, the azimuthal quantum number
in the new nomenclature will be represented by nf*. The reason for
this will be discussed during the derivation.
In addition to the above, the current nomenclature lists a number of "term"
letters for values of the orbital quantum number, l. The first five of these
are:-
| Quantum Number l | 0 | 1 | 2 | 3 | 4 |
| Term | s | p | d | f | g |
This term scheme is adopted, but in relation to the azimuthal quantum number
nf (and nf *), in the new nomenclature. In this paper only
the first three quantum numbers, n, nf, (and nf*), and nr will be involved. The other numbers resulting from the effects due to
spin will appear in subsequent papers.
2.2 Justification of the Quantization Criteria & Determination of Permitted Orbits.
To begin this analysis, consider again the energy component of [1],
Eq.(2.1). If this is to represent the orbital energy of a bound electron in
an atom, for that electron orbit to be stable, it is necessary for the bound
energy to be constant over an entire single orbit, e.g. there can be no net
energy loss or gain. Thus for such a case, if the energy in [1], Eq.(2.1) is
to be constant, then in [1], Eq.(2.15), fv must also be constant over an
entire orbit. In turn, this means that in a simple re-arrangement of [1],
Eqs.(2.24) and (2.26),
the product vlsv must be similarly constant.
and where
v is the electron's orbital velocity.
lsv is the electron's orbital spatial matter wave wavelength.
c is the velocity of light.
fv is the electrons spatial - temporal matter wave frequency.
It is noted that (2.1) appears to invoke the fictitious spatial "phase
velocity" of the electron matter wave, viz [1], Eq.(2.19). However, although
the quantity c2/v appears in (2.1) it is only via a re-arrangement of the relationships between real parameters and is therefore acceptable as a
mathematical descriptor.
In a stable elliptic orbit, the orbital velocity v cannot be constant because
the distance of the orbiting electron from the central nucleus is
continuously changing. Consequently for (2.1) to be constant for such an
orbit, lsv while being single valued over an entire orbit ,
must however vary proportionately in precise inverse harmony to the
variation in v within the orbit. This then ensures that the elliptical orbit
is stable. In circular orbits, the distance of the electron from the central
nucleus is constant and so the orbital velocity is constant. Thus in this
case lsv is not only single valued over a complete orbit, but
also exactly constant throughout it. The so called "pendulum orbits" are
discussed at the end of this Section.
Now, to justify the criterion of quantisation, the single valuedness of
lsv over a complete orbit, inserting the component parts of
v for a basic elliptic orbit in (2.1) gives after minor re-arrangement
|
lsv = |
c2
fv
|
|
æ è
|
×
r
|
+wf2 r 2 |
ö ø
|
-1/2
|
|
| (2.2) |
where
r is the radial distance of the electron from the nucleus.
| ×
r is the radial velocity of the electron in its orbit. |
wf is the angular rate of the electron in its orbit.
Now, in any elliptic orbit it is well known that
|
|
|
|
|
|
| ×
r
|
= | wf Lesinf ( 1+ecosf )2
| |
|
| |
| (2.3) |
Where
f is the angular position of the radius vector from some axis origin.
L is the semi latus rectum of the elliptic orbit.
e is the eccentricity of the orbit.
Substitution of (2.3) into (2.2) gives after minor reduction
|
lsv = |
c2
fv
|
|
m0 L
Mf
|
( 1+e2+2ecosf )-1/2 |
| (2.4) |
Where
Mf is the angular momentum of the rest mass of the electron and is
constant by the law of conservation.
m0 is the rest mass of the electron.
On the RHS of (2.4) the only variable is the angular position so that it is
clear that over a complete orbit
Eq.(2.5) states that over the orbital path length of a stable orbit the
orbiting electron's matter wave wavelength is an integer number. Therefore
the criterion of quantisation is now linked to the requirement that, within
a stable orbit, the bound energy of the orbiting electron must be constant.
Accordingly, the criterion of quantisation is thus proved to be a necessary
and sufficient condition for the stability of a basic electron orbit. The
variability of lsv within the orbit is also clearly visible in
(2.4).
If e = 0 then (2.4) becomes
and is constant throughout the complete orbit. This is the electron matter
wave wavelength for circular orbits, (r º L).
In the case of the pendulum orbits, in (2.4) L = 0 and therefore lsv = 0. Accordingly from [1], Eq.() fsv becomes infinite,
which from [1], Eq.(2.26) requires that the orbital velocity v also becomes
infinite. This contravenes the criterion of existence within the
Relativistic Space-Time Domain D0, and is a sufficient proof for the
exclusion of the pendulum orbits. Note that for fsv to be infinite would
also necessitate infinite orbital energy.
In (2.4) if e = 1, it becomes
|
lsv = |
m0 c2L
Ö2 fv Mf
|
( secf )1/2 |
| (2.7) |
The orbit is parabolic and f varies from -(p-d) to
+(p-d). Quantisation does not apply because the orbit is not
closed. The same comment applies to hyperbolic orbits, (e >
1).
2.3 Quantisation of the Bohr/Sommerfeld Atom.
In view of the results of the preceding Section, it is now permissible to
apply the quantisation process to relativistically modified electron orbits
to resurrect the Bohr/Sommerfeld theory of atomic structure.
Rewriting [1], Eq.(2.18) as
where h is Planck's constant.
Because the wavelength is to be quantised for all orbit path lengths, both
sides of (2.8) are integrated over the orbital path length to give
where l is the length of the orbit path, and m the energy mass of the electron.
On the LHS if l is to be an integral number of wavelengths then (2.9) can be
written
Where n is an integer, the principle quantum number of the orbit. In (2.9)
and (2.10) the circled integral sign indicates integration over the complete
path of the orbit. It is (2.10) which will later be used as the source
equation for the sample quantisation of a number of permitted orbits.
To show that the above derivation leads to the same quantisation results as
in the original Bohr theory, it is sufficient to demonstrate that (2.10)
leads to the original quantisation rules as propounded by Niels Bohr.
With
insertion of this into (2.10) and expansion of the RHS gives
|
nh = | ó (ç) õ
| m |
æ è
|
×
r
|
2
|
+wf 2 r 2 |
ö ø
|
dt |
| (2.12) |
Splitting the RHS of (2.12) into two terms then gives
|
nh = | ó (ç) õ
| m |
×
r
|
dr+ | ó (ç) õ
| mwf r 2df |
| (2.13) |
which can clearly be written
|
nh = | ó (ç) õ
| Mr* dr+ | ó (ç) õ
| Mf * df |
| (2.14) |
where
Mr* is the radial momentum of the relativistically mass corrected
electron.
Mf * is the angular momentum of the relativistically mass
corrected electron.
Eq.(2.14) is identical to the original quantisation rules of Niels Bohr with
the minor exception that the momentum terms are corrected for the
relativistic mass increase of the electron. Eq.(2.14) is perhaps the most
elegant way of representing the quantisation process but simpler analysis
results from the use of (2.10) as in Section 3 below.
2.4 Orbital Energy Levels.
In order to derive quantised orbital energy levels, an energy expression
suitable for use in the process is required. To derive the form required
here, use is made of the solution to the orbital equation of motion, which
has been effected in [2]. The result however, requires considerable
preliminary analysis before insertion into the orbital energy derivation
process. For clarity, this preliminary analysis is relegated to Appendix A,
Section A.1, the results of which are used in the following process.
Starting with Einstein's energy/momentum equation as stated at [1],
Eq.(2.29), the bound energy of the electron is
|
Eor = m0 c2 |
æ è
|
1+ |
M 2
m02 c2
|
ö ø
|
1/2
|
- m0 c2 - |
Ze2
r
|
|
| (2.15) |
where
Eor is the orbital or bound energy of the electron.
M is the spatial momentum of the electron in its orbit.
Z is the atomic number of the atom.
e is electronic charge.
It should be noted that although the atomic number has been included in this
analysis, only hydrogen, (Z = 1), will be considered in detail when calculating
spectra.
Via binomial expansion, retaining only second order relativistic terms,
(2.15) reduces to
|
Eor = |
m0 v2
2
|
+ |
3
8
|
|
m0 v4
c2
|
- |
Ze2
L
|
( 1+ecosj ) |
| (2.16) |
where
L is the relativistically corrected orbit semi-latus rectum.
e is the relativistically corrected orbit eccentricity.
and where (A.3) has been inserted for r. An expression for v is now required.
From (A.3)
|
|
×
r
|
= |
dr
dt
|
= |
drdj
djdt
|
= |
wj Lesinj
( 1+ecosj )2
|
|
| (2.17) |
The angular velocity of the electron is wf r which from (A.3) and (A.14) is
|
wf r= |
wj L
( 1+ecosj )
|
|
æ è
|
1+ |
Z 2e4
c2Mj *2
|
ö ø
|
1/2
|
|
| (2.18) |
So that from (2.17) and (2.18)
|
v2 = |
×
r
|
2
|
+ wf 2 r 2 = |
wj 2 L 2e 2 sin2j
( 1+ecosj )4
|
+ |
wj2 L2
( 1+ecosj )2
|
|
æ è
|
1+ |
Z 2e4
c2Mj *2
|
ö ø
|
|
| (2.19) |
which with (A.14) reduces to
|
v2 = |
Mj *2
m02 L2
|
|
ì í
î
|
1 + 2ecosj + e2 + |
Z 2e4
c2Mj *2
|
( 1+ecosj )2 |
ü ý
þ
|
|
æ è
|
1- |
v2
c2
|
ö ø
|
|
| (2.20) |
Solving (2.20) for v2 gives
|
v2 = |
|
|
Mj *2
m02 L2
|
|
ì í
î
|
1 + 2ecosj + e2+ |
Z 2e4
c2Mj *2
|
( 1+ecosj )2 |
ü ý
þ
|
|
|
|
é ë
|
1+ |
Mj *2
m02 c2L2
|
|
ì í
î
|
1 + 2ecosj + e2+ |
Z 2e4
c2Mj *2
|
( 1+ecosj )2 |
ü ý
þ
|
ù û
|
|
|
|
| (2.21) |
Substitution of this into (2.16) gives for the orbital energy, after some
reduction including binomial expansion to relativistic second order
|
|
|
Eor = |
Mj *2
2m02 L2
|
|
ì í
î
|
1 + 2ecosj + e2 + |
Z 2e4
c2Mj *2
|
( 1+ecosj )2 |
ü ý
þ
| | | - |
Mj *4
8m03 c2L4
|
{ 1 + 2ecosj + e2 }2- |
Ze2
L
|
( 1+ecosj ) |
|
|
|
|
|
| (2.22) |
Now, substituting for L from (A.14) gives, again after some reduction
|
|
|
Eor = |
Z2e4
2Mj *2
|
{ 1 + 2ecosj + e2 }- |
Z2e4
Mj *2
|
( 1+ecosj ) |
+ |
Z4e8
c2Mj *4
|
|
ì í
î
|
1
2
|
( 1 + ecosj )2 - |
1
2
|
( ecosj + e2 )( 1 - e2 ) - |
1
8
|
( 1 + 2ecosj + e2 )2 |
ü ý
þ
|
|
|
|
| (2.23) |
which finally reduces to
|
Eor = - |
Z2e4m0 ( 1-e2 )
2Mj *2
|
|
æ è
|
1- |
3
4
|
|
Z2e4
c2Mj *2
|
( 1-e2 ) |
ö ø
|
|
| (2.24) |
This expression for the orbital energy can now be quantised for all
permitted orbits by inserting the appropriate expression for Mj *2/( 1-e2 ). Non-relativistically corrected orbits can be
treated by letting c ® ¥, and circular orbits by putting
e = 0. Eq.(2.24) leads directly to the expanded version of
Sommerfeld's equation for relativistically mass corrected elliptic orbits as
will be shown in Section 3.5.
P2 Version 2.0.1
Ó
P.G.Bass, April 2008
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