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XYLENE POWER LTD.

**INTRODUCTION:**

This web page reviews the concepts of heat, temperature and thermal radiation. Temperature is expressed in terms of radiation density and radiation spectral distribution.

**HEAT:**

A high school definition of heat is "energy related to molecular motion", but that definition is not helpful in addressing thermal radiation issues. A more general definition of heat is "thermal energy". A change in temperature, together with rest mass density, volume and heat capacity collectively indicate a change in contained thermal energy, also known as a change in enthalpy.

The heat capacities of materials vary and are somewhat temperature and pressure dependent. Typical heat capacities and atomic weights for solid elemental metals are set out in the following table.

ELEMENT | HEAT CAPACITY (J / gm-C) | ATOMIC WEIGHT | ROW PRODUCT |
---|---|---|---|

Lithium | 3.559 | 6.95 | 24.735 |

Beryllium | 1.825 | 9.012 | 16.446 |

Sodium | 1.214 | 22.990 | 27.910 |

Magnesium | 1.047 | 24.305 | 25.447 |

Aluminum | 0.921 | 26.981 | 24.849 |

Potassium | 0.753 | 39.098 | 29.441 |

Calcium | 0.628 | 40.078 | 25.169 |

Nickel | 0.502 | 58.693 | 29.463 |

Iron | 0.461 | 55.845 | 25.744 |

Zinc | 0.376 | 65.38 | 24.582 |

Tin | 0.217 | 118.710 | 25.76 |

Lead | 0.126 | 207.2 | 26.107 |

In a vacuum the incremental heat added to an object (AKA change in enthalpy) with rest mass is given by:

(Heat Added) = (Heat Capacity) X (Mass) X (Rise in Temperature)

The row products in the above table indicate that the product:

(Heat Capacity in J / gm-C) X (Atomic Weight in gm / mole) X (1 mole / 6.023 X 10^23 atoms)

= (Heat Capacity in J / mole)

is nearly constant for most metals.

Hence, neglecting thermal radiation, the amount of heat added to a metal object is approximately the product of:

(Number of Atoms present) X (rise in temperature).

Thus a rise in temperature causes a similar rise in thermal energy in all metal atoms.

In general **temperature is an indication of nearly equally distributed thermal kinetic energy per atom**. This energy is known as lattice thermal energy.

However, there is another component of thermal energy known as thermal radiation.

**THERMAL RADIATION:**

Thermal radiation exists in a vacuum and has no rest mass. Thermal radiation is thermal photon energy.

**THERMAL ENERGY:**

1. Thermal energy consists of lattice thermal energy plus thermal photon energy.

2. Except in a high vacuum the lattice thermal energy of a material is usually very large compared to the thermal photon energy.

3. The lattice thermal energy primarily consists of molecular kinetic energy. Changes in lattice potential energy and lattice kinetic energy are closely coupled.

4. The thermal photon energy consists of the energy quanta of photons. Photons and excited electrons are closely coupled.

5. There is weak coupling between the two sepatate closely coupled energy classes. Lattice vibrations move the electron spheromaks into a slightly different external magnetic field environments which couples energy onto the electrons. Alternatively absorbed photon energy may excite electrons which couples energy back to the lattice. The atomic nuclei may also directly absorb and emit a small fraction of the photons.

**TEMPERATURE:**

In science temperature is an indication of the average energy per thermal photon. In reality for a material there may be two temperatures. There is the lattice temperature which, after allowance for material phase changes, indicates average kinetic energy of molecules. There is the photon temperature which indicates average electromagnetic energy of thermal photons. Photons and molecules exchange energy primarily via electrons. At thermal equilibrium the lattice temperature equals the photon temperature. However, under nonequilibrium conditions these two temperatures may be quite different. For example, if a plasma is excited by a micro second long pulse of electromagnetic radiation for a brief period after the excitation pulse (~ 1 ms) the electrons in a plasma may have a much higher temperature than the ions.

Lattice temperature is indicated by thermal expansion (eg a mercury thermometer) or change in pressure of a contained gas. In this respect two convenient reference temperatures are the freezing point of water (273.15 K, 0 C, 32 F) and the boiling point of water (100.0 C at 1 atmosphere pressure). However, thermal expansion does not convey any concept of radiative heat transfer.

A small portion of the thermal excitation energy exists as photons. The photons exchange energy with electrons. A measurement of the thermal radiation spectrum indicates the photon temperature. At room temperature the thermal emission radiation spectrum is in the far infrared. Solar radiation is primarily thermal emission photons by the sun, which has an effective surface temperature of about 5778 degrees K.

In our local universe the vacuum of outer space is filled with photons which have an average temperature of 2.73 degrees K.

Note that even though the photon energy per unit volume is relatively small compared to the lattice energy of a material, because photons propagate at the speed of light the photon energy flux can be large.

**PHASE CHANGE:**

Materials exist in solid, liquid, gas and plasma phases. When a material transitions from its solid phase to its liquid phase it can absorb a lot of heat while hardly changing in photon temperature. This absorbed heat is known as the latent heat of fusion.

When a material transitions from its liquid phase to its gas phase the material can absorb a lot of heat while hardly changing in photon temperature. This absorbed heat is known as the latent heat of vaporization.

A mercury thermometer, which operates by thermal expansion of liquid mercury, only gives valid readings in the temperature range where mercury is liquid. A platinum resistance temperature sensor only gives valid readings in the temperature range where platinum is solid.

Thus many temperature indicating instruments only give valid results within a temperature range where there is no phase change in the sensing element.

**THERMAL RADIATION:**

Consider the following:

1. Heat can flow across a vacuum barrier confirming the existence of radiative heat transfer.

2. A vacuum isolated object is at the same temperature as its environment when the absorbed thermal radiation equals the emitted thermal radiation.

3. At thermal equilibrium the change in the object's total energy Et with respect to time t is zero, or:

dEt / dt = 0.

4. An object is at zero absolute temperature (0 degrees K) if it emits no radiation.

5. Hence temperature is an indication of an object's total energy with respect to the object's total energy when it emits no radiation.

6. Heat spontaneously flows across a vacuum from objects at high temperatures to objects at lower temperatures.

7. Hence the rate of thermal radiation emission increases as temperature increases.

8. The rate of heat transfer across a vacuum barrier is less for reflective object and container surfaces than for black object and container surfaces.

9. Hence the rate of thermal radiation emission is a function of temperature and surface reflectivity.

10. Recall that the temperature of an object is independent of the number of atoms or molecules in the object.

11. Recall that for an object composed of only one atomic or molecular type, temperature is an indication of average thermal kinetic energy per atom or per molecule.

12. The photon temperature of an object can be precisely obtained by analysis of the object's emitted thermal radiation spectrum.

13. The primary source of thermal radiation photons is thermally excited electron spheromaks.

14. Thermal radiation also occurs when excited nuclei emit radiation photons.

15. Consider an evacuated container. When the evacuated space is at thermal equilibrium with the container walls the vacuum is filled with photons emitted from the container's inside walls and absorbed by these walls. If a uniform spherical object is inserted into the container it reflects, absorbs and emits photons with spherical symmetry.

16. The thermal radiation has a temperature dependent energy density and pressure. Planck calculated the photon energy density and frequency distribution as a function of absolute temperature.

17. Electron and proton spheromak energies follow:

E = h F

where:

h = 6.62607004 X 10^-34 m^2 kg / s

is known as the Planck Constant.

18. Due to the properties of the spheromaks from which the thermal photons are emitted and absorbed the energy Ep of each radiated photon is related to the photon frequency Fp via the expression:

Ep = h Fp

19. Bose-Einstein statistics give the relative fraction of photons with energies between Ep and (Ep + dEp) as:

(dEp / [Exp(Ep / K T) - 1]) = (h dF / [Exp(h F / K T) - 1])

whete:

K = Boltzmann Constant

= 1.38064852 X 10^-23 m^2 kg s^-2 K^-1

and

T = absolute temperature

Note that energy quantization prevents Ep going to zero which keeps the Bose-Einstein function finite at low values of Ep.

20. Thus although there is a high density of states at high photon energies (high photon frequencies} the probability of high energy (high photon frequency) states being occupied is very low, which limits the maximum radiation energy density at any particular temperature.

21. We need to portray the relastionship between photon temperature, radiation frequency and radiation energy density.

22. An advantage of expressing temperature in terms of photon radiation instead of in terms of molecular kinetic energy is that with suitable instrumentation radiation emitted by distant objects can be precisely measured.

**TEMPERATURE MEASUREMENT VIA ANALYSIS OF THE EMITTED PHOTON SPECTRUM:**

A clear advantage of measuring temperature via the thermal emission photon spectrum is that it the measurement is valid regardless of the phase of the emitting material. However, confusion can arise when the surface of the emitting material is at a different photon temperature than the bulk of the material. This problem occurs with atmospheres around planets and stars.

Another source of confusion is variations in material emissivity and temperature. For example if the emissivity of the surface of a planet that has no atmosphere is not uniform and the planets surface is scanned by a satellite, it is difficult to distinguish changes in surface temperature from changes in surface emissivity. Changes in emissivity with frequency cause additional confusion. Most devices that measure temperature via analysis of the thermal emission photon spectrum implicitly assume that in the region being studied the temperature is uniform and that the emissivity is uniform and independent of frequency.

**PLANCK LAW:**

Planck's law states that:

I(Fp, T) = {2 h Fp^3 / C^2} / {[Exp(h Fp / K T)] - 1}

where:

I(Fp,T) is the power (the energy per unit time) of frequency Fp radiation emitted per unit area of emitting surface in the normal direction per unit solid angle per unit frequency by a black body at temperature T, also known as spectral radiance;

h is the Planck constant = 6.62607004 × 10-34 m2 kg / s;

C is the speed of light in a vacuum = 299 792 458 m / s;

K is the Boltzmann constant = 1.38064852 × 10-23 m2 kg s-2 K-1;

Fp is the frequency of the electromagnetic radiation in Hz;

T is the absolute temperature of the body in degrees K.

Note that the Planck Law is only true for uniform temperature bodies and hence requires modification for planets and stars surrounded by atmospheres that at high altitudes are at a lower temperature than the planet or star surface. The Planck law is only valid for the temperature at the point of photon emission. If received photons originate from points at different temperatures analysis of the data becomes complicated.

Photons emitted into space from Earth's atmosphere preferentially originate from locations in the atmosphere where the temperature is just below 273.15 K, the freezing point of water. The issue of the change in Earth's planetary Bond albedo (solar reflectivity) as this temperature rises above 273.15 K has enormous practical significance.

**DERIVATION OF PLANCK LAW:**

The essence of the Planck Law is that at any particular temperature at thermal equilibrium there is a corresponding photon energy density and a corresponding photon spectral distribution. This web page is primarily concerned with finding that energy density and spectral distribution.

The presentation herein relies on the reader having some familiarity with Bose-Einstein statistics, the concept of statistical occupancy of different energy states, boundary conditions applicable to electromagnetic radiation in a conducting cavity, orthogonal Fourier functions, solid angle geometry, electron spheromaks, the Planck constant and vector notation.

Consider a cavity inside a solid. Assume that the cavity has electrically and thermally conducting walls. The cavity is filled with electromagnetic radiation in thermal equilibrium at temperature T.

The total energy in the cavity with respect to the ground state can be found by summing over the contained energies of all allowed single photon states. This can easily be done because the mathematical formulation allows integration from photon energy Ep = 0 to Ep = infinity. To calculate the energy in the cavity we need to evaluate how many photon states there are at each photon energy. The probability of a photon state being occupied is given by Bose-Einstein statistics.

It turns out that each photon state is an orthogonal Fourier component.

The photon energy density U(T) in a cavity of volume V is given by:

U(T) V = Integral over all possible energies of:

[Photon Energy Ep]

X [Number of photon states per unit energy in the cavity at energy Ep]

X [Probability of photon state occupancy between Energy Ep and energy (Ep + dEp)]

= Integral from E = 0 to E = infinity of:

{[Ep] [g(Ep) dEp] / [Exp(E / K T) - 1]}

In this expression:

Ep = photon energy;

g(Ep) = number of photon states per unit energy at energy Ep;

{dEp / [Exp(Ep / K T) - 1]} = Statistical mechanics Bose-Einstein relative probability of a photon energy state being occupied between energy Ep and (Ep + dEp) at temperature T.

**DENSITY OF PHOTON STATES:**

From special relativity:

Ep^2 = |Pp|^2 C^2 + Mo^2 C^4

For a photon Mo = 0

Hence a photon with energy Ep has momentum **Pp** given by:

**|Pp|** = Ep / C

However, **Pp** has many different possible propagation angles.

Assume that photon momentum states are uniformly distributed through positive momentum space and that the separation between adjacent momentum states is constant. This assumtion is equivalent to assuming that each momentum state contains an orthogonal Fourier component of the total photon momentum.

**Px** = momentum state spacing along the x axis;

**Py** = momentum state spacing along the y axis;

**Pz** = momentum state spacing along the Z axis.

Then a momentum state is defined by:

**Pp**(Nx. Ny, Nz) = Nx **Px** + Ny **Py** + Nz **Pz**

where:

Nx, Ny, Nz are positive integers;

and

**|Px| = |Py| = |Pz| = |Po|**

Ep(Nx, Ny, Nz) = |Pp(Nx, Ny, Nz)| C

= [Nx^2 **Px^2** + Ny^2 **Py^2** + Nz^2 **Pz^2**]^0.5 C

= [Nx^2 + Ny^2 + Nz^2]^0.5 **|Po|** C

where:

**|Po|** = Eo / C

Part of the adjacent momentum state separation is due to photon energy. The remaining momentum state separation is due to photon propagation angle.

Then the momentum state vectors **Pp**(Nx, Ny, Nz) take discrete equally spaced values. Then:

**|Pp|** = [(Nx Px)^2 + (Ny Py)^2 + (Nz Pz)^2]^0.5

= [Nx^2 + Ny^2 + Nz^2]^0.5 **|Po|**

= N **|Po|**

where:

N = [Nx^2 + Ny^2 + Nz^2]^0.5

The density of momentum states in momentum space is:

1 state / **|Po|**^3

Recall that:

Ep = **|Pp|** C

or

**|Pp|** = Ep / C

Define:

Eo = **|Po|** C

Assume that due to photon polarization there are 2 photon states per momentum state. Hence for every momentum vector **Pp** with integer components larger than or equal to zero, there are two photon states. This means that the number of photon states in a certain region of momentum space is twice the number of momentum states in that region.

The discrete states in a particular energy range in momentum space lie between |Pp| and (|Pp| + d|Pp|).

Because Nx, Ny, Nz are positive, this momentum space shell spans an octant (1 / 8) of a sphere. The number of photon states g(E) dE, in an energy range dE, is thus given by:

g(Ep) dEp = 2 (1 / 8) (4 Pi **|Pp|**^2 d**|Pp|**)(1 / **|Po|**^3)

= Pi (Ep / C)^2 d(Ep / C)[1 / (Eo / C)^3]

= Pi Ep^2 dEp / Eo^3

This is the number of photon states between energy Ep and (Ep + dEp)

Hence the density of states per unit energy is:

**g(Ep) = Pi Ep^2 / Eo^3**

Note that the density of states is very low at low energies. Even though the Bose-Einstein function makes the relative probability of state occupancy very high at low energies the low density of states at low energies forces the product:

(state energy) X (density of states) X (relative probability of state occupancy)

to zero at low energies.

**CAVITY ENERGY:**

The photon energy in the cavity with respect to the ground state is given by:

U(T) V = Integral from Ep = 0 to Ep = infinity of:

Ep [Pi Ep^2 / Eo^3] { dEp / [Exp(Ep / KT) - 1]}

= Integral from Ep = 0 to Ep = infinity of:

[Pi Ep^3 / Eo^3] { dEp / [Exp(Ep / KT) - 1]}

Define:

X = Ep / KT

= (h Fp) / (K T)

and

dX = dEp / KT

Then:

U(T) V = Integral from Ep = 0 to Ep = infinity of:

[Pi Ep^3 / Eo^3] { dEp / [Exp(Ep / KT) - 1]}

= Integral from X = 0 to X = infinity of:

[K T]^4 [Pi X^3 / Eo^3] { dX / [Exp(X) - 1]}

This expression has units of energy. That energy is distributed over a cavity volume V.

**CAVITY VOLUME:**

Eo = h Fo = h C / Lamdao

or

Lamdao = h C / Eo

The cavity wall boundary conditions on the thermal equilibrium standing wave photon require that cavity length L satisfy:

L = Lamdao / 2 = h C / 2 Eo

The cavity volume V is:

V = L^3

= [h C / 2 Eo]^3

**CAVITY PHOTON ENERGY DENSITY:**

Hence the average photon energy density in the cavity is:

**U(T)** = [U(T) V] / V

= Integral from X = 0 to X = infinity of:

[K T]^4 [Pi X^3 dX / Eo^3] {1 / [Exp(X) - 1]} / [h C / 2 Eo]^3

= {8 [KT]^4 Pi / (h C)^3}Integral from X = 0 to X = infinity of:

{X^3 dX / [Exp(X) - 1]}

= {8 [K T]^4 Pi / (h C)^3} {Pi^4 / 15}

= **8 [K T]^4 [Pi^5 / 15] / (h C)^3**

This equation gives the cavity photon energy density as a function of temperature.

Recall that:

U(T) V = Integral from E = 0 to E = infinity of:

[Pi E^3 / Eo^3] { dE / [Exp(E / KT) - 1]}

and

V = [h C / 2 Eo]^3
Hence:

U(T) = [U(T) V] / V

= Integral from Ep = 0 to Ep = infinity of:

[Pi Ep^3 / Eo^3] { dEp / [Exp(Ep / KT) - 1]} / [h C / 2 Eo]^3

= Integral from Ep = 0 to Ep = infinity of:

8 [Pi Ep^3] { dEp / [Exp(Ep / KT) - 1]} / [h C]^3

Substitue:

Ep = h Fp

and

dEp = h dFp

to get:

U(T) =
= Integral from Fp = 0 to Fp = infinity of:

8 [Pi (h Fp)^3 h] { dFp / [Exp(h Fp / KT) - 1]} / [h C]^3

Hence:

**dU = 8 [Pi Fp^3 h / C^3] { dFp / [Exp(h Fp / KT) - 1]}**

This equation gives the cavity photon energy density as a function of frequency and temperature.

**CAVITY PHOTON ENERGY EMISSION:**

Consider energy emitted via a small hole in the cavity. The spectrum of this emitted radiation is known as "Black Body Radiation" because the spectrum is not affected by the material surface reflectivity. If all the exiting energy propagated forward the radiation intensity in the aperture would be:

(radiation density in cavity) C.

However, in reality the photon radiation propagates omni-directionally so that the forward component of the radiation is:

I(Fp, T) dFp = (radiation density in cavity) C / 4 Pi sterradians

= dU(Fp, T) C (1 / 4 Pi)

= 8 [Pi Fp^3 h dFp / C^3] { 1 / [Exp(h Fp / KT) - 1]} C (1 / 4 Pi)

= {2 h Fp^3 dFp / C^2} / {[Exp(h Fp / K T)] - 1}

This equation is known as the Planck Law. It has units of watts / m^2-sterradian

The Planck Law is:

**I(Fp, T) = {2 h Fp^3 / C^2} / {[Exp(h Fp / K T)] - 1}**

By definition the Stefan Boltzmann constant is:

**Cb = [2 Pi^5 / 15] [K^4 / C^2 h^3]
= 5.670400 X 10^-8 J / s-m^2-K^4**

Hence U(T) can be written more compactly using the Stefan–Boltzmann constant Cb, giving:

**U(T)** = 8 [K T]^4 [Pi^5 / 15] / (h C)^3

= **[4 Cb / C] T^4**

The constant:

**[4 Cb / C]**

is sometimes called the radiation constant. This constant allows easy calculation of radiation energy contained in a volume of space at a particular temperature.

**NUMERICAL EXAMPLE:**

Find the cavity radiation energy density at 270 degrees K:

[U|T = 270 deg K] = [4 Cb / C] T^4

= [4 X 5.670400 X 10^-8 J / s-m^2-K^4 / (3 X 10^8 m / s)] X [270 K]^4

= [4 X 5.670400 X 10^-8 J / m^3] X [(2.7)^4 / 3]

= **4.017977 X 10^-6 J / m^3**

This radiation energy density does not seem large but the associated radiant power flux is substantial because part of this radiation energy propagates away into space at the speed of light = 3 X 10^8 m / s.

**WIEN'S DISPLACEMENT LAW:**

Wien's displacement law shows how the spectrum of black-body radiation at any temperature is related to the spectrum at any other temperature. If we know the shape of the spectrum at one temperature, we can calculate the shape at any other temperature. Spectral intensity can be expressed as a function of wavelength or of frequency.

A consequence of Wien's displacement law is that the wavelength Lamdam at which the intensity per unit wavelength of the radiation produced by a black body is at a maximum is a function only of the temperature:

Lamdam = {b / T}

where the constant b, known as Wien's displacement constant, is:

b = 2.8977729(17) × 10-3 K m.

Planck's law was also stated above as a function of frequency. The frequency Fm of maximum intensity is given by:

Fm = T X 58.8 GHz / K

**STEFAN BOLTZMANN LAW:**

The Stefan–Boltzmann law states that the power emitted per unit area from the surface of a black body is directly proportional to the fourth power of the body's absolute temperature:

**J = Cb T^4**,

where:

J is the total power radiated per unit area,

T is the absolute temperature

and

**Cb = 5.670400 X 10-8 W m-2 K-4
is the Stefan–Boltzmann constant**.

**STEFAN BOLTZMANN LAW DERIVATION:**

Recall that Planck's Law is:

I(Fp, T) = {2 h Fp^3 / C^2} / {[Exp(h Fp / K T)] - 1}

The Stefan Boltzmann law follows from integrating I(Fp ,T) over frequency and solid angle:

J = (Integral from Fp = 0 to Fp = infinity) dF (Integral dOmega cos(theta) I(Fp, T))

where:

(Integral dOmega cos(theta)

= (Integral from Phi = 0 to Phi = 2 Pi) d(Phi)) (Integral from Theta = 0 to Theta = Pi / 2) d(Theta) sin(Theta) cos(Theta)

= Pi

The cos(Theta) factor appears since we are considering the radiation in the direction normal to the surface.

The solid angle integral extends over the full Phi = 0 to Phi = 2 Pi in azimuth and over the polar angle Theta = 0 to Theta = Pi / 2.

I(Fp,T) is independent of angles theta and Phi and passes through the solid angle integral. Inserting the formula for I(Fp ,T)} gives:

J = {[2 Pi (K T)^4] / C^2 h^3]} {Integral from X = 0 to X = infinity of {X^3 dX / [(Exp X) - 1]}}

where:

X = h Fp / K T

is unitless.

The integral over X has the value Pi^4 / 15}, which gives:

**J = Cb T^4**

where:

**Cb = [2 (Pi^5 / 15)(K^4)] / (C^2 h^3)
= 5.670400 X 10^-8 W / m^2-K^4**

This web page last updated June 24, 2017.

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