2.0  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.

NameCurrent
Nomenclature
ValueNewValue
Principlen1 to ¥n1 to ¥
Azimuthalk1 to nnf1 to n
Orbitall0 to (n - 1) Not Used -
Radialn/n - knrn - nf
Spins s + 1/2
s- 1/2
nsp± 1/2
Innerj 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 l01234
Termspdfg

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),


vlsv = c2

fv
(2.1)

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 = L

( 1+ecosf )
so    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


lsv |f = 2p = lsv |f = 0
(2.5)

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


lsv = rm0 c2

fv Mf
(2.6)

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


h

lsv
= mv
(2.8)

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


hl

lsv
=ó
(ç)
õ

mvdl
(2.9)

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


nh =ó
(ç)
õ

mvdl
(2.10)

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


dl = vdt
(2.11)

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

On to the Next Section:- Quantisation of Simple Orbits

Back to the Introduction to this Paper:- Basic Orbits

Back to the Home Page for this Site:- Home