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The Voigt elastic approximation assumes uniform strain. Differentiating its averaged strain energy density gives the averaged local stress. For linear elasticity the predicted elastic stiffness tensor is $C_V=⟨C⟩$. The uniform strain is an admissible affine displacement trial field, so this gives an upper elastic energy bound for convex local energy.

A channel supporting ballistic electron transport carries incident populations set by different source and drain chemical potentials, rather than an everywhere-equilibrated local distribution with an Ohmic voltage gradient. Its electrostatic barrier responds self-consistently to contacts, gates and electrostatic screening. A symmetric rigid-barrier model places reservoir energies at $E_F\pm eV/2$ relative to the barrier. Asymmetric partition or bias-dependent transmission changes the weights in the differential electrical conductance, and must be included when extracting an energy scale.

Historical terminology for electrical effects supplied by electrochemical cells. The source supplies energy through chemical changes; the resulting electric charge and electric current obey the same electrical laws as charge supplied by other means.

Waldan K. Kwong coauthored research on chlorophyll.^[ref]

Chlorophyll is a family of molecules that absorb light for photosynthesis. In chloroplasts, chlorophyll works with proteins in thylakoid membranes; absorbing light initiates energy capture rather than directly constructing a sugar. See OpenStax Biology 2e, 8.2: photosynthetic pigments.

A trial domain pattern costs wall energy ${\gamma }_w{A}_w$ and can release stray energy $\Delta U$. For a stable uniform ground state, ${\gamma }_w{A}_w\ge \Delta U$ within that trial model. Substituting the entire initial stray energy assumes that it is nearly all removed; a numerical lower bound independent of the domain geometry does not follow from single-domain observation alone.

For a Newtonian fluid and a flat wall with $0<b<\infty$, the Navier slip boundary condition is equivalent to a tangential wall-on-fluid tractionThe sign expresses resisting friction: ${\partial }_{n}u$ uses the inward unit normal, whereas the wall-on-fluid traction uses the outward unit normal of the fluid domain. The irreversible loss of mechanical energy per unit wall area and time isFor two tangential directions replace $u_{\mathrm{rel}}^2$ by the squared Euclidean norm of relative tangential velocity. At a moving wall this relative-velocity loss must be distinguished from the power supplied by the wall's motion. Bulk viscous dissipation also remains present. A finite slip length models reduced interfacial resistance, without declaring every boundary ideal or removing dynamic viscosity.

The limiting loss depends on how the flow is driven. In Couette flow with a slipping lower wall,It tends to zero for both $b\to 0$ and $b\to \infty$ at fixed $H$ and $U$. At $b=0$ impose the no-slip boundary condition directly, rather than dividing by zero. In planar Poiseuille flow with equal wall slip at fixed $G$, each wall instead dissipates $G^{2}b{H}^2/(4\mu )$, which grows with $b$ because relative velocity grows. The bulk loss per unit width is $G^2{H}^3/(12\mu )$; adding both wall losses gives $Gq$, the pressure work per unit channel length and width. This energy balance shows why small friction coefficients do not guarantee small losses under every driving constraint.

Walter Kohn and Pierre Hohenberg established a foundation for density functional theory: under their ground-state assumptions, the electron density determines the external scalar potential up to an additive constant. They formulated the ground-state energy as a universal density functional plus the external-potential contribution, with a variational principle selecting the physical density. This replaces the full many-electron wave function as the basic variable by a function of only three spatial coordinates. The theorem establishes the framework, rather than providing an explicit exact functional for practical computation.^[ref]

A Wannier-Mott exciton has an internal wave function extending over many unit cells. Its simplest model assumes a three-dimensional bulk crystal, approximately parabolic valence band and conduction band, positive isotropic scalar effective masses $m_e^{\ast },m_h^{\ast }$, a constant scalar relative permittivity ${ϵ}_r$, and a dilute pair population. Replace microscopic crystal forces by those effective masses and dielectric screening, and neglect exchange corrections and coupling to phonons. These assumptions must hold on the spatial and energy scales of the particular exciton.

With relative coordinate $\mathbf{r}={\mathbf{r}}_e-{\mathbf{r}}_h$, the internal Hamiltonian operator is the three-dimensional hydrogen atom problem with a reduced mass and a screened Coulomb potential:Here $e$ is the elementary charge, ${ϵ}_0$ the vacuum permittivity, and $\hslash$ the reduced Planck constant. The internal energy eigenvalues, radius scale, and exciton binding energies areThe principal quantum number is $n=1,2,\dots$. This reduction and these scales are derived in Excitons in Semiconductor Quantum Dots by Matjaž Humar (§3, printed pp. 5–6, equations (13)–(26)).

To check the scales by dimensional analysis, write $C=e^2/(4\pi {ϵ}_0{ϵ}_r)$, which has units of energy times length. Then $a_B^{\ast }={\hslash }^2/(\mu C)$ is a length and $R^{\ast }=\mu C^2/(2{\hslash }^2)$ is an energy. Rescaling $r=a_B^{\ast }\rho$ makes $H_{\mathrm{rel}}/R^{\ast }=-{\nabla }_{\rho }^2-2/\rho$, the dimensionless hydrogen atom operator. The Bohr radius $a_B^{\ast }$ is a wave function scale, not the radius of a classical orbit; for this model's lowest internal bound state, the mean separation is $3a_B^{\ast }/2$.

For the diagrams' hypothetical inputs $m_e^{\ast }=0.10m_0$, $m_h^{\ast }=0.40m_0$, ${ϵ}_r=10$ and $E_g=1.500\mathrm{eV}$, where $m_0$ is the free electron mass, independent substitution gives $\mu =0.080m_0$, $a_B^{\ast }\simeq 6.615\mathrm{nm}$ and $R^{\ast }\simeq 10.885\mathrm{meV}$. Here electronvolts express energy. The exciton binding energies for $n=1,2,3$ are approximately $10.885$, $2.721$ and $1.209\mathrm{meV}$. These are model calculations, not measured material parameters. The large-radius approximation additionally requires $a_B^{\ast }$ to be much larger than the crystal's unit cell length scale. In a thin layer, with anisotropic effective masses, or with spatially varying dielectric screening, this three-dimensional formula is not generally valid.

A water-equivalent material is a material whose relevant interaction with ionizing radiation approximates that of water under specified conditions. For a water phantom, the comparison concerns energy absorption and scattering in the measurement geometry. It is not a statement that the material merely has a density near that of water, or that equivalence at one energy applies at every other energy.^[ref]

For a narrow monoenergetic photon beam, the linear attenuation coefficient satisfieswhere $\rho$ is the mass density and $\mu /\rho$ the mass attenuation coefficient. Equal densities leave the mass interaction coefficients unconstrained. Predicting absorbed dose also involves how transferred energy is deposited, for which the mass energy-absorption coefficient is relevant; the attenuation of primary photons alone is not the complete scattering and deposition problem. For charged particles, the corresponding comparison also involves stopping power.

For an original toy calculation, stipulate equal densities but linear attenuation coefficients ${\mu }_w=0.05\mathrm{c}{\mathrm{m}}^{-1}$ and ${\mu }_m=0.08\mathrm{c}{\mathrm{m}}^{-1}$ at one chosen photon energy. For $t=10\mathrm{cm}$, the unscattered fractions in the Beer-Lambert law areThe substitute transmits only $e^{-0.3}\approx 0.74082$ times the unscattered intensity of the reference, despite identical density. These coefficients are stipulated model inputs, not tabulated data for real water or a named plastic. Matching even this transmission at one energy would not establish equal absorbed dose throughout a larger scattering object. Energy dependence of water equivalence is therefore part of any meaningful equivalence specification.

A focused physical comparison places the same characterized detector in reference water and in a candidate slab assembly, with controlled material thickness, irradiation geometry and detector position. Record density and composition as well as detector response over the intended radiation conditions. Slab gaps and changes in surrounding scattering material can confound the comparison; the primary IAEA discussion explicitly treats material variability and the approximate nature of plastic-to-water scaling.^[ref]

Choose approximate atomic weights $A_{\mathrm{r}}(\mathrm{H})=1.008$ and $A_{\mathrm{r}}(\mathrm{O})=15.999$, and use $M_{\mathrm{u}}\approx 1\mathrm{g}\mathrm{mo}{\mathrm{l}}^{-1}$. The chemical formula ${\mathrm{H}}_2\mathrm{O}$ then gives water molar massThese are deliberately chosen rounded inputs, not exact atomic weights or a universal value for every water sample. Different isotopic abundances, notably those in heavy water, change the mean molar mass; chemical formula alone does not specify them. Adding atomic weights also neglects the tiny mass change associated with chemical bond energies, immaterial at this rounding precision.

For an illustrative pure water sample of mass $4.50375\mathrm{g}$, this convention givesThe count refers to water molecules. Their hydrogen chemical atom count is approximately $2N=3.01107038\times 10^{23}$, and their oxygen chemical atom count is approximately $N$. The mean mass per water molecule is $M/N_{\mathrm{A}}\approx 2.99146\times 10^{-26}\mathrm{kg}$. Extra displayed digits expose the arithmetic; they do not imply that the sample composition or mass was measured that precisely.

The same conversion makes stoichiometry a mass calculation. For the chemical equation $2{\mathrm{H}}_2+{\mathrm{O}}_2\to 2{\mathrm{H}}_2\mathrm{O}$, complete conversion of $0.250000\mathrm{mol}$ of molecular hydrogen and $0.125000\mathrm{mol}$ of molecular oxygen gives $0.250000\mathrm{mol}$ of water. With the chosen approximate atomic weights, the reactant masses are $0.50400\mathrm{g}$ and $3.99975\mathrm{g}$, summing to $4.50375\mathrm{g}$. The $2:1:2$ ratio belongs to molecule counts and amount of substance, not to masses; this bookkeeping neglects the much smaller reaction energy contribution to mass.

A water phantom is a water-filled reference object used to measure how a radiation field deposits energy under specified, reproducible conditions. In radiation dosimetry, a detector can be positioned at controlled depths and lateral locations inside the water. The measured quantity is related to absorbed dose in that reference medium; the tank is not a complete anatomical model of a patient.^[ref]

The surrounding medium matters physically. Photons and charged particles can scatter, attenuate and transfer energy before it is collected locally. An empty holder, a small isolated water sample and a large water tank need not produce identical fields at a detector. The named IAEA edition treats both water as reference material and the margins of scattering material around a measurement region. A water-equivalent material must be compared in relevant absorption and scattering properties, not identified by similar bulk density alone.^[ref]

A practical apparatus combines a tank, a positionable ionization chamber or another characterized detector, a readout and a way to define the water surface. For example, PTW's MP1 description specifies one-dimensional detector travel, levelling supports and fill marks. Its depth-positioning mechanism supports a depth-dose curve; one mechanical coordinate is not itself a full three-dimensional scan.^[ref]

An original position-error model shows why the reference coordinates matter. At a fixed depth, stipulate a lateral absorbed dose profileA $1\mathrm{mm}$ displacement from $x=20\mathrm{mm}$ changes the dose ratio toThe same displacement from the centre gives $D(1)/D(0)\simeq 0.99875$. Thus the same absolute positioning error can produce about $5\%$ variation on a gradient and only $0.125\%$ at the centre of this stipulated profile. These are mathematical examples, not measured beam characteristics or equipment accuracy claims.

An ionization chamber also samples a finite sensitive volume, so detector volume averaging can differ from a point value of $D(x)$. Converting its collected electric charge to absorbed dose requires the applicable measurement calibration and measurement model, as described in medical physicist. Changing the tank position does not remove a detector's intrinsic spatial response.

Comparisons should therefore identify the water surface, detector reference point, irradiation geometry, water conditions and background treatment. The IAEA discussion of waterproof sleeves and chamber positioning illustrates why the detector and its surrounding hardware are part of the measurement configuration.^[ref]

The watt is the SI unit of power, one joule per second. Joule heating at $12.5\mathrm{W}$ transfers $125\mathrm{J}$ of energy over a time of $10\mathrm{s}$ if that power stays constant. ^[ref].

A wave is a spatially organized disturbance whose evolution can transmit a pattern and energy through space. Shake one end of a stretched mechanical string: the displacement travels along it while each small piece mainly moves up and down. In a small-amplitude acoustic wave, nearby fluid elements similarly oscillate about their mean positions while the pressure disturbance travels onward. Transport of a wave therefore need not mean bulk transport of the material carrying it.

For a one-dimensional nondispersive travelling wave, $u(x,t)=f(x-ct)$ keeps its shape while moving at wave speed $c$. A sinusoidal example has wavelength $\lambda$ and frequency $f=c/\lambda$. Oppositely travelling disturbances can instead form a standing wave. Interference follows from the superposition principle when the governing equations are linear; nonlinear waves can change shape and interact more strongly. Measuring arrival time, frequency and wave amplitude makes waves useful probes of both a source and the medium between source and receiver.

Wave absorption transfers energy from a propagating wave to other degrees of freedom of a medium. For a plane wave that is a monochromatic wave, with amplitude proportional to $e^{i(k^{\prime }+i{k}^{\prime \prime })z}$ and $k^{\prime \prime }>0$, its wave intensity decreases as $I(z)=I(0)e^{-2k^{\prime \prime }z}$. The intensity absorption coefficient is therefore $2k^{\prime \prime }$ when this loss is due to absorption. A decreasing transmitted wave intensity can also result from wave reflection or wave scattering, which redistribute energy rather than necessarily converting it into heat.

For a small-amplitude conservative wave packet in a slowly varying fluid flow, its intrinsic energy divided by intrinsic frequency is transported along its group velocity, with the basic advection added in the laboratory frame. A stationary background conserves laboratory angular frequency, but a changing mean velocity changes the intrinsic one through the Doppler effect; intrinsic energy alone need not be conserved. Geometrical spreading and dissipation enter the action-flux balance.

Wave attenuation is a reduction of a chosen wave component as it travels through sea ice. An amplitude coefficient $\alpha$ corresponds to an energy coefficient $2\alpha$. Wave scattering at a planar interface can remove energy from the forward wave without dissipating total energy; viscous dissipation, collisions and internal ice losses irreversibly convert mechanical energy to heat.

For a smooth phase $\Theta$, define local wavenumber $k={\Theta }_x$ and local angular frequency $\omega =-{\Theta }_t$. Equality of mixed derivatives gives $k_t+{\omega }_x=0$. Dividing by $2\pi$ expresses conservation of signed crest count with density $k/(2\pi )$ and flux $\omega /(2\pi )$. When a homogeneous local dispersion relation gives $\omega =\omega (k)$, the equation becomes $k_t+v_g(k)k_x=0$; its characteristic curves move at the group velocity. This phase compatibility is distinct from energy or wave-action conservation.

For a real semilinear wave equation $u_{tt}-\Delta u+V^{\prime }(u)=0$, its energy density and energy flux areMultiply the equation by $u_t$ and use the product rule to obtain the local balance ${\partial }_{t}e+\mathrm{div}j=0$. On a fixed regular domain $\Omega$ this givesThus total wave energy is conserved when the boundary term vanishes: for example homogeneous Dirichlet boundary conditions, homogeneous Neumann boundary conditions, paired periodic boundary conditions, or suitable decay on all of space. A driven boundary can instead inject energy.^[ref]

For the linear wave equation, take $V=0$ and obtain $E_{\mathrm{lin}}=\frac{1}{2}\int (u_t^2+|\nabla u{|}^2)dx$. A defocusing potential such as $V(u)=|u{|}^{p+1}/(p+1)$ adds a nonnegative term. A focusing negative potential still obeys the balance law but need not control positive norms; conservation and positivity are separate properties.

Wave focusing brings contributions from an extended incident field into a smaller region so that their wave phases reinforce there. A converging lens redirects a wavefront; a phased source array instead sets the relative wave phases at emission. In either case, the field near the focus is the superposition of the arriving contributions.

An ideal geometrical ray description can concentrate rays to a point, but diffraction gives a finite focal spot for a finite aperture. For an aperture of size $D$ and focal distance $f$, its characteristic transverse scale is of order $\lambda f/D$, with a coefficient depending on aperture shape and the width convention. Focusing increases local wave intensity by concentrating available power; it does not create energy. Blocking part of the aperture or changing its wave phase changes both the focal spot and the surrounding pattern. These effects can be tested by scanning a small detector across the focal plane.

For a propagating branch of an ideal vacuum-filled rectangular electromagnetic waveguide, the phase velocity tracks constant wave phase along the axis, whereas the group velocity describes a sufficiently narrow, weakly distorted wave packet. Using ${\omega }^2=c^2{\beta }^2+{\omega }_c^2$ givesThus $v_{\mathrm{ph}}>c$, $0<v_g<c$, and $v_{\mathrm{ph}}{v}_g=c^2$. Differentiating the dispersion relation proves the second formula; dividing it by ${\beta }^2$ proves the first. This is the same mathematical structure as Klein-Gordon packet velocities. In the stipulated $f=1.25f_c$ example,Over $0.30\mathrm{m}$, the corresponding narrow-envelope delay is $(0.50\mathrm{m})/c$, approximately $1.668\mathrm{ns}$. Timing a carrier wave crest would give $0.6004\mathrm{ns}$; it does not time the arrival of a newly introduced message.

There is an independent energy check. For the forward ${\mathrm{TE}}_{10}$ fields, the average axial Poynting vector is $⟨S_z⟩=\beta |E_y{|}^2/(2{\mu }_0\omega )$. Integrating across the guide gives average power $P$ and average electromagnetic energy per unit length $U^{\prime }$:The transverse sine and cosine squared each integrate to $a/2$; ${\beta }^2+(\pi /a{)}^2={\omega }^2/c^2$ then makes the integrated electric and magnetic contributions to $U^{\prime }$ equal. The axial energy transport therefore agrees with the group velocity in this ideal model.

As $\omega \downarrow {\omega }_c$, $v_g\to 0$ and $v_{\mathrm{ph}}\to \infty$; exactly at cutoff $\omega /\beta$ is undefined. Strong wave dispersion close to cutoff also limits the narrow-packet approximation. Neither a large phase velocity nor a pulse peak establishes superluminal information velocity; front velocity asks a separate causal question. In a uniform filling with constant positive permittivity $\epsilon$ and magnetic permeability $\mu$, replace $c$ by $u=1/\sqrt{\epsilon \mu }$, giving $v_{\mathrm{ph}}{v}_g=u^2$. Frequency-dependent material response or significant loss requires differentiating the actual dispersion relation, so this product is not universal.