Defining equation (physics)

Defining equations in physics are equations which define new quantities in terms of fundamental ones. Quantities follow the same heirachy as the chosen system of units; fundamental quantities have defined base units, from which other quantities May Be derived. This article uses the current SI system of units, not natural or characteristic units.

For the common nomenclature for fundamental base quantities used in this article see: Physical quantity.

Classical Mechanics

Mass and Inertia

Main Articles: Inertia, Mass

Mass can be considered to be inertial or gravitational.

Inertial mass is associated with a body's inertia to maintain uniform momentum, while acted on by zero resultant force. Similarly inertial mass corresponds to the moment of inertia of a body to maintain uniform angular momentum, while acted on by zero resultant torque AbOUT any axis through any spatial point.

Gravitational mass is associated with the cause of gravitational attraction.

Inertial and gravitational mass are found to be equal by Newton's 3rd Law, later by Einstein's Principle of Equivalence (for Acceleration).

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|Minertiaa = Mgravityg   |}

Masses occur as discrete or continuous distributions. "Discrete mass" and "continuum mass" are not different quantities; the only differance is the calculation either as summation (discrete) or integration (continuous). Centre of mass is not to be confused with centre of gravity (see Center of mass).

Quantity (Common Name/s)

(Common) Symbol/s

Defining Equation

SI Units

Dimension

Mass density of dimension n
(Vn = n-space)
n = 1 for linear mass density,
n = 2 for surface mass density,
n = 3 for volume mass density,
etc

linear mass density λ  ,
surface mass density σ  ,
volume mass density ρ  ,
no general symbol for
any dimension

n-space mass density:
$\rho_n = \frac{ \partial ^n m}{ \partial x_n \cdots \partial x_2 \partial x_1} = \frac{\partial m}{ \partial V_n} \,\!$
special cases are:
$\lambda = \frac{ \partial m}{ \partial x} \,\!$
$\sigma = \frac{ \partial^2 m}{ \partial x_2 \partial x_1} = \frac{ \partial^2 m}{ \partial S} \,\!$
$\rho = \frac{ \partial^3 m}{ \partial x_3 \partial x_2 \partial x_1} = \frac{ \partial m}{ \partial V} \,\!$

kg m-n

[M][L]-n

Total discrete mass

m, M

M = ∑imi  

kg m

[M][L]

Total continuum mass

m, M

n-space mass density
M = ∫ρndnx = ∫⋯∫∫ρndx1dx2⋯dxn  
Special cases are:
M = ∫λdx  
M = ∫σdA = ∬σdx1dx2  
M = ∫ρdV = ∭ρdx1dx2dx3  

kg

[M]

Moment of Mass

m (No common symbol)

Point mass: m = rm  
Descrete masses about an axis xi  :
$\mathbf{m} = \sum_{i=1}^N \mathbf{r}_\mathrm{i} m_i \,\!$
Continuum of mass about an axis xi  :
m = ∫ρ(r)xidr  

kg m

[M][L]

Centre of Mass

rcom
(Symbols vary enormously)

ith moment of mass mi = rimi   Discrete masses:
$\mathbf{r}_\mathrm{com} = \frac{1}{M}\sum_i \mathbf{r}_\mathrm{i} m_i = \frac{1}{M}\sum_i \mathbf{m}_\mathrm{i} \,\!$
Mass continuum:
$\mathbf{r}_\mathrm{com} = \frac{1}{M}\int \mathbf{r} \mathrm{d}^n m = \frac{1}{M}\int \mathbf{r} \rho_n \mathrm{d}^n x = \frac{1}{M}\int \mathbf{r} \mathrm{d}\mathbf{m} \,\!$

m

[L]

2-Body Reduced Mass

m12, μ
Pair of masses = m1 and m2

μ = (m1m2)/(m1+m2)  

kg

[M][L]2

Moment of Inertia (MOI)

I

Discrete Masses:
I = ∑imi ⋅ ri = ∑i|ri|2m  
Mass continuum:
I = ∫|r|2dm = ∫r ⋅ dm = ∫|r|2ρndnx  

kg m2 s−1

[M][L]2

Derived Kinematic Quantities

Main Articles: Kinematics, Cross product

For the inclusion of the scalar angle of rotational position θ, it is necessary to include a normal vector    to the plane containing and defined by the position vector and tangential direction of rotation, so that the vector equations hold.

Using the basis vectors for polar coordinates, which are , θ̂, ϕ̂  , the unit normal is  =  × θ̂  .

Quantity (Common Name/s)

(Common) Symbol/s

Defining Equation

SI Units

Dimension

Velocity

v

v = dr/dt  

m s−1

[L][T]−1

Acceleration

a

$\mathbf{a} = \frac{\mathrm{d} \mathbf{v}}{\mathrm{d} t } = \mathrm{d}^2 \mathbf{v}/\mathrm{d} t^2 \,\!$

m s−2

[L][T]−2

Jerk

j

j = da/dt = d3v/dt3  

m s−3

[L][T]−3

Angular Velocity

ω

ω = (dθ/dt)  

rad s−1

[T]−1

Angular Acceleration

α

α = dω/dt = (d2θ/dt2)  

rad s−2

[L][T]−2

Derived Dynamic Quantities

Quantity (Common Name/s)

(Common) Symbol/s

Defining Equation

SI Units

Dimension

Momentum

p

p = mv  

kg m s−1

[M][L][T]−1

Force

F

$\mathbf{F} = \frac{\mathrm{d} \mathbf{p}}{\mathrm{d} t } \,\!$

N = kg m s−2

[M][L][T]−2

Impulse

Δp, I

I = Δp = ∫t1t2Fdt  

kg m s−1

[M][L][T]−1

Angular Momentum about a position point R  

L, J, S

L = (rR) × p  

kg m2 s−1

[M][L]2[T]−1

Total, Spin and Orbital

Angular Momentum

L, J, S

Ltotal = Lspin + Lorbital  

kg m2 s−1

[M][L]2[T]−1

Moment of a Force
about a position point R,

Torque

τ, M

$\boldsymbol{\tau} = \left ( \mathbf{r} - \mathbf{R} \right ) \times \mathbf{F} = \frac{\mathrm{d} \mathbf{L}}{\mathrm{d} t } \,\!$

N m = kg m2 s−2

[M][L]2[T]−2

Angular Impulse

ΔL No common symbol

ΔL = ∫t1t2Ldt  

kg m2 s−1

[M][L]2[T]−1

Coefficient of Restitution

e, ε

$e = \frac{\left | \mathbf{v} \right | _\mathrm{separation}}{\left | \mathbf{v} \right | _\mathrm{approach}} \,\!$

usually 0 ≤ e ≤ 1  

but it is possible that e ≥ 1  

Dimensionless

Dimensionless

General Energy Definitions

Main Article: Mechanical energy

Quantity (Common Name/s)

(Common) Symbol/s

Defining Equation

SI Units

Dimension

Mechanical Work due

to a Resultant Force

W

W = ∫CF ⋅ dr  

J = N m = kg m2 s−2

[M][L]2[T]−2

Work done ON mechanical

system, Work done BY

WON, WBY

ΔWON =  − ΔWBY  

J = N m = kg m2 s−2

[M][L]2[T]−2

Potential Energy

φ, Φ, U, V, Ep

ΔW =  − ΔV  

J = N m = kg m2 s−2

[M][L]2[T]−2

Mechanical Power

P

$P = \frac{\mathrm{d}E}{\mathrm{d}t} \,\!$

W = J s−1

[M][L]2[T]−3

Lagrangian

L

L = T − V  

J

[M][L]2[T]−2

Action

S

S = ∫Ldt  

J s

[M][L]2[T]−1

Potential Energy and Work

Every conservative force has a potential energy. By following two principles one can consistently assign a non-relative value to U:

  • Wherever the force is zero, its potential energy is defined to be zero as well.
  • Whenever the force does work, potential energy is lost.

Transport Mechanics

Here    is a unit vector normal to the cross-section surface at the cross section considered.

Quantity (Common Name/s)

'''(Common)

Symbol/s'''

Defining Equation

SI Units

Dimension

Flow Velocity Vector Field

u

u = u(x,t)  

m s−1

[L][T]−1

Mass Current,

Mass flow rate

Im

Im = ∂m/∂t  

kg s−1

[M][T]−1

Mass Current Density

jm

jm = (∂Im/∂A) = (∂2m/∂At)  

kg m−2 s−1

[M][L]−2[T]−1

Momentum Current

Ip

Ip = ∂|p|/∂t  

kg m s−2

[M][L][T]−2

Momentum Current Density

jp

jp = (∂Ip/∂A) = ∂2p/∂At  

kg m s−2

[M][L][T]−2

Properties of Matter

Stress and strain

Quantity (Common Name/s)

(Common) Symbol/s

Definining Equation

SI Units

Dimension

General Stress

σ  

σ = F/A  

F may be any force applied to area A

Pa = N m−2

[M] [T] [L]−1

General Strain

ϵ  

ϵ = ΔD/D  

D = dimension (length, area, volume)

ΔD   = change in dimension

dimensionless

dimensionless

General Elastic Modulus

Emod  

Emod = σ/ϵ  

Pa = N m−2

[M] [T] [L]−1

Yield Strength/

  

Ultimate Tensile Strength

  

Young's Modulus

E, Y  

$Y = \frac{F L}{A \Delta L} \,\!$

Pa = N m−2

[M] [T] [L]−1

Shear Modulus

G  

G = Δx/L  

Pa = N m−2

[M] [T] [L]−1

Bulk Modulus

B  

$B = \frac{P}{\Delta V / V}\,\!$

Pa = N m−2

[M] [T] [L]−1

Thermodynamics

Thermodynamic Quantities

State Properties for Systems

Main articles: List of thermodynamic properties, Thermodynamic Potential, Free entropy

Quantity (Common Name/s)

(Common Symbol/s)

Defining Equation

SI Units

Dimension

Number of Molecules

N

dimensionless

dimensionless

Temperature

T

K

[Θ]

Heat Energy

Q, q

J

[M][L]2[T]−2

Latent Heat

QL

J

[M][L]2[T]−2

Entropy

S

J K−1

[M][L]2[T]−2 [Θ]−1

Negentropy

J

J K−1

[M][L]2[T]−2 [Θ]−1

Internal Energy

Sum of all total energies which

constitute the system

U

U = ∑iEi

J

[M][L]2[T]−2

Enthalpy

H

H = U + pV  

J

[M][L]2[T]−2

Partition Function

Z

dimensionless

dimensionless

Inverse Temperature

β

β = 1/kBT  

J-1

[T]2[M]-1[L]-2

Gibbs Free Energy

G

G = H − TS  

J

[M][L]2[T]−2

Chemical Potential (of

component i in a mixture)

μi

μi = (∂U/∂Ni)Ni ≠ j, S, V  

(Ni, S, V must all be constant)

J

[M][L]2[T]−2

Electrochemical Potential (of

component i in a mixture)

μ̄i  

μ̄i = μ − zeNAϕ  

φ = local electrostatic potential

(see below also)

zi = valency (charge)

of the ion i

J

[M][L]2[T]−2

Helmholtz Free Energy

A, F

A = U − TS  

J

[M][L]2[T]−2

Landeu Potential, Landau Free Energy

Ω

Ω = U − TS − μN  

J

[M][L]2[T]−2

Grand Potential

ΦG

ΦG = E − TS − μN  

J

[M][L]2[T]−2

Massieu Potential,

Helmholtz free entropy

Φ

Φ = S − U/T  

J K−1

[M][L]2[T]−2 [Θ]−1

Planck potential,

Gibbs free entropy

Ξ

Ξ = Φ − pV/T  

J K−1

[M][L]2[T]−2 [Θ]−1

Thermal Properties of Matter

Main Articles: Heat capacity, Thermal expansion,

Quantity (Common Name/s)

(Common Symbol/s)

Defining Equation

SI Units

Dimension

General Heat Capacity

C

C = ∂Q/∂T  

J K −1

[M][L]2[T]−2 [Θ]−1

Heat Capacity (isobaric)

Cp

Cp = ∂Q/∂T  

J K −1

[M][L]2[T]−2 [Θ]−1

Specific Heat Capacity (isobaric)

Cmp

Cmp = ∂2Q/∂mT  

J kg−1 K−1

[L]2[T]−2 [Θ]−1

Molar Specific Heat

Capacity (isobaric)

Cnp

Cnp = ∂2Q/∂nT  

J K −1 mol−1

[M][L]2[T]−2 [Θ]−1 [N]−1

Heat Capacity (isochoric)

CV

CV = ∂Q/∂T  

J K −1

[M][L]2[T]−2 [Θ]−1

Specific Heat Capacity (isochoric)

CmV

CmV = ∂2Q/∂mT  

J kg−1 K−1

[L]2[T]−2 [Θ]−1

Molar Specific Heat

Capacity (isochoric)

CnV

CnV = ∂2Q/∂nT  

J K −1 mol−1

[M][L]2[T]−2 [Θ]−1 [N]−1

Specific Latent Heat

L

L = ∂Q/∂m  

J kg−1

[L]2[T]−2

Ratio of Isobaric to

Isochoric Heat Capacity,

Adiabatic Index

γ

γ = Cp/CV = cp/cV = Cmp/CmV  

dimensionless

dimensionless

Linear Coefficient of Thermal Expansion

α

L/∂t = αL  

K−1

[Θ]−1

Volume Coefficient of Thermal Expansion

3α, γ

V/∂t = 3αV  

K−1

[Θ]−1

Thermal Transfer

Main articles: Thermal conductivity

Quantity (Common Name/s)

(Common Symbol/s)

Defining Equation

SI Units

Dimension

Temperature Gradient

T (No standard symbol)

T = ∇T  

K m−1

[Θ][L]−1

Thermal Conduction Rate, Thermal

Current, Thermal/Heat Flux

P

P = ∂q/∂t  

W = J s−1

[M] [L]2 [T]−2

Thermal Intensity

I

I = ∂P/∂A = ∂2q/∂At  

W m−2

[M] [T]−3

Thermal/Heat Flux Density

(vector analogue of Thermal

Intensity above)

q

q = I = 2q/∂At  

W m−2

[M] [T]−3

Thermal Conductance

U

U = λ/δx  

W m−2 K−1

[M] [T]−3 [Θ]

Thermal Conductivity

κ, K, λ

λ =  − P/(A⋅∇T)  

W m−1 K−1

[M] [L] [T]−2 [Θ]−1

Thermal Resistance

R

R = 1/U = Δx/λ  

m2 K W−1

[L] [T]2 [Θ]1 [M]−1

Emissivity Coefficient

ε

Can only be found from experiment

0 ≤ ϵ ≤ 1  

ϵ = 0   for perfect reflector

ϵ = 1   for perfect absorber

(true black body)

dimensionless

dimensionless

Waves

General Fundamental Quantities

Main articles: Transverse wave, Longitudinal wave

Quantity (common name/s)

(Common) symbol/s

SI units

Dimension

Number of wave cycles

N

dimensionless

dimensionless

(Transverse) Displacement

y, r  

m

[L]

(Transverse) Displacement amplitude

A, B, C, x0, xm

m

[L]

(Transverse) Velocity amplitude

V, v0 , vm

m s−1

[L][T]−1

(Transverse) Acceleration Amplitude

A, a0, am

m s−2

[L][T]−2

(Longnitudinal) Displacement

x, r  

m

[L]

Period

T

s

[T]

Wavelength

λ

m

[L]

Phase angle

δ, ε, φ

rad

dimensionless

General Derived Quantities

Quantity (Common Name/s)

(Common) Symbol/s

Defining Equation

SI Units

Dimension

(Transverse) Velocity

v  , vt

v = ∂r/∂t  

m s−1

[L][T]−1

(Transverse) Acceleration

a  , at

v = ∂v/∂t = ∂2r/∂t2  

m s−2

[L][T]−2

Path Length Difference

L, ΔL, Δx, Δr  

Δr = (r)2 − (r)1  

m

[L]

(Longnitudinal) Velocity

v, vp  

v = Δr/Δt  

m s−1

[L][T]−1

Frequency

f

General definition:

f = ΔN/Δt  

Commonly N is set to 1 cycle, seting t = T = time

period for 1 cycle gives the more useful definition:

f = 1/T  

Hz = s−1

[T]−1

Angular Frequency/ Pulsatance

ω

ω = 2πf = 2π/T  

Hz = s−1

[T]−1

Time Delay, Time Lag/Lead

Δt

Δt = t2 − t1  

s

[T]

Scalar Wavenumber

k

Two definitions are used:

k = 2π/λ  

k = 1/λ  

In the formalism which follows, only the first

definition is used.

m−1

[L]−1

Vector Wavenumber,

k-vector, Wave vector

k

Again two definitions are possible:

k = (2π/λ)  

k = (1/λ)  

In the formalism which follows, only the first

definition is used.

m−1

[L]−1

Phase Differance

δ, Δε, Δϕ

Δϕ = ϕ2 − ϕ1  

rad

dimensionless

Phase

Φ (No standard symbol)

Φ = r − vt + Δr/N = λ  

Φ = kr − ωt + ϕ = 2πN  

Physically;

wave popagation in +r direction

r > 0 ⇒ ω < 0  

wave popagation in -r direction

r < 0 ⇒ ω > 0  

Phase angle can lag if: ϕ > 0  

or lead if: ϕ < 0  

rad

dimensionless

Relation between space, time, angle analogues used to describe the phase Φ:

$\frac{\Delta r}{\lambda} = \frac{\Delta t}{T} = \frac{\phi}{2\pi} \,\!$

Damping Parameters, Forces and Torques

Main articles: Damping

Quantity (Common Name/s)

(Common) Symbol/s

Defining Equation

SI Units

Dimension

Spring Constant (Hooke's Law)

k, K, κ, kH

kH = ΔF/Δx  

N m−1

[M][T]−2

Damping Coefficient

b

b =  − ΔFd/Δv  

N s m−1

[L][T]−1

Damping Force

Fd

N

[M][L][T]−2

Damping Ratio

ζ

ζ = b/bcritical  

dimensionless

dimensionless

Logarithmic decrement

δ

δ = (1/n)ln |A0/An|  

A0   is any amplitude, An   is the

amplitude n successive peaks

later from A0  , where A0 > An  

dimensionless

dimensionless

Torsion Constant

κ

κ =  − Δτ/Δθ  

N m rad−1

[M][L]2[T]−2

Damping Torque

τd

N m

[M][L]2[T]−2

Rotational Damping Coefficient

β

β =  − τd/(dθ/dt)  

N m s rad−1

[M][L]2[T]−1

Acoustics

Quantity (Common Name/s)

(Common) Symbol/s

Definining Equation

SI Units

Dimension

Linear Mass Density

μ

$\mu = \frac{\partial m}{\partial t}\,\!$

kg m-1

[M] [L]-1

Sound Level

β

$\beta = \left ( 10 \mathrm{dB} \right ) \log \left | \frac{I}{I_0} \right | \,\!$

dimensionless

dimensionless

Gravitation

A common misconseption occurs between centre of mass and centre of gravity. They are defined in simalar ways but are not exactly the same quantity. Centre of mass is the mathematical descrition of placing all the mass in the region considered to one position, centre of gravity is a real physical quantity, the point of a body where the gravitational force acts. They are only equal if and only if the external gravitational field is uniform.

Contrary to the strong analogy between (classical) gravitation and electrostatics, there are no "centre of charge" or "centre of electrostatic attraction" analogues.

Quantity Name

(Common) Symbol/s

Defining Equation

SI Units

Dimension

Centre of Gravity

rcog  

(Symbols can vary

enourmously)

ith moment of mass mi = rimi  

Centre of gravity for a descrete masses

$\mathbf{r}_\mathrm{cog} = \frac{1}{M \left | \mathbf{g} \left ( \mathbf{r}_i \right ) \right |}\sum_i \mathbf{m}_i \left | \mathbf{g} \left ( \mathbf{r}_i \right ) \right | \,\!$

$= \frac{1}{M \left | \mathbf{g} \left ( \mathbf{r}_\mathrm{cog} \right ) \right |}\sum_i \mathbf{r}_i m_i \left | \mathbf{g} \left ( \mathbf{r}_i \right ) \right | \,\!$

Centre of a gravity for a continuum of mass

$\mathbf{r}_\mathrm{cog} = \frac{1}{M \left | \mathbf{g} \left ( \mathbf{r}_\mathrm{cog} \right ) \right |}\int \left | \mathbf{g} \left ( \mathbf{r} \right ) \right |\mathrm{d}\mathbf{m} \,\!$

$= \frac{1}{M \left | \mathbf{g} \left ( \mathbf{r}_\mathrm{cog} \right ) \right |}\int \mathbf{r} \left | \mathbf{g} \left ( \mathbf{r} \right ) \right | \mathrm{d}^n m \,\!$

$= \frac{1}{M \left | \mathbf{g} \left ( \mathbf{r}_\mathrm{cog} \right ) \right |}\int \mathbf{r} \rho_n \left | \mathbf{g} \left ( \mathbf{r} \right ) \right | \mathrm{d}^n x \,\!$

m

[L]

Standard GravitationParameter of a Mass

μ  

μ = Gm  

N m2 kg−1

[L]3 [T]−2

Gravitational Field, Field

Strength, Potential Gradient,

Acceleration

g  

$\mathbf{g} = \frac{\mathbf{F}}{m} \,\!$

N kg−1 = m s−2

[L][T]−2

Gravitational Flux

ΦG  

ΦG = ∫Sg ⋅ dA  

m3 s−2

[L]3[T]−2

Absolute Gravitational Potential

Φ, ϕ, U, V  

$U = - \frac{W_{\infty r}}{m} = - \frac{1}{m} \int_\infty^{r} \mathbf{F} \cdot \mathrm{d}\mathbf{r} = - \int_\infty^{r} \mathbf{g} \cdot \mathrm{d}\mathbf{r} \,\!$

J kg−1

[L]2[T]−2

Gravitational Potential Differance

ΔΦ, Δϕ, ΔU, ΔV  

$\Delta U = - \frac{W}{m} = - \frac{1}{m} \int_{r_1}^{r_2} \mathbf{F} \cdot \mathrm{d}\mathbf{r} = - \int_{r_1}^{r_2} \mathbf{g} \cdot \mathrm{d}\mathbf{r} \,\!$

J kg−1

[L]2[T]−2

Gravitational Potential Energy

Ep  

Ep =  − Wr  

J

[M][L]2[T]−2

Gravitational Torsion Field

Ω  

$\nabla \times \mathbf{g} = \frac{\partial \boldsymbol{\Omega}}{\partial t} \,\!$

F = m(v×Ω)  

Hz = s−1

[T]−1

Gravitational Torsion Flux

ΦΩ  

ΦΩ = ∫SΩ ⋅ dA  

N m s kg−1 = m2 s−1

[M]2 [T]−1

Gravitomagnetic Field

ξ  

Hz = s−1

[T]−1

Gravitomagnetic Flux

Φξ  

Φξ = ∫Sξ ⋅ dA  

N m s kg−1 = m2 s−1

[M]2 [T]−1

Gravitomagnetic Vector Potential

h  

ξ = ∇ × h  

m s−1

[M] [T]−1

Electromagnetism

Electric Quantities

Charge

Quantity (Common Name/s)

(Common) Symbol/s

Defining Equation

SI Units

Dimension

Electric Charge (any amount)

q, Q

C = A s

[I][T]

Electric charge density of dimension n

(Vn   = n-space)

n = 1 for linear mass density,

n = 2 for surface mass density,

n = 3 for volume mass density,

etc

linear charge density λ,

surface charge density σ,

volume charge density ρ,

no general symbol for

any dimension

n-space charge density:

ρn = ∂nm/∂xn⋯∂x2x1 = ∂m/∂Vn  

special cases are:

λ = ∂m/∂x  

σ = ∂2m/∂x2x1 = ∂2m/∂S  

ρ = ∂3m/∂x3x2x1 = ∂m/∂V  

C m-n

[I][T][L]-n

Total descrete charge

Q

Q = ∑iqi  

C

[I][T]

Total continuum charge

Q

n-space charge density

Q = ∫ρndnx = ∫⋯∫∫ρndx1dx2⋯dxn  

special cases are:

Q = ∫λdx  

Q = ∫σdA = ∬σdx1dx2  

Q = ∫ρdV = ∭ρdx1dx2dx3  

C

[I][T]

Capacitance

C

C = ∂q/∂V  

F = C V−1

Electric Current

I

I = dq/dt  

A

[I]

Current Density

J

J = (∂I/∂A)  

A m−2

[I][L]−2

Displacement current

Id

Id = ϵ0(∂ΦE/∂t)  

A

[I]

Charge Carrier Drift Speed

vd

m s−1

[L][T]−1

Electric Fields

Quantity (Common Name/s)

(Common) Symbol/s

Defining Equation

SI Units

Dimension

Electric Field, Field Strength,

Flux Density, Potential Gradient

E

E = F/q  

N C−1 = V m−1

[M][L][T]−3[I]−1

Electric Flux

ΦE

ΦE = ∫SE ⋅ dA  

N m2 C−1

[M][L]3[T]−3[I]−1

Relative Permittivity
(AKA Dielectric constant)

εr

F m−1

[I]2 [T]4 [M]−1 [L]−3).

Absolute Electric Permittivity;

ε

ϵ = ϵrϵ0  

F m−1

[I]2 [T]4 [M]−1 [L]−3).

Electric Displacement Field

D

D = E/ϵ  

C m−2

[I][T][L]−2

Electric Displacement Flux

ΦD

ΦD = ∫SD ⋅ dA  

C

[I][T]

Electric Dipole Moment

p

p = 2qa  

a   is the charge separation

directed from -ve to +ve charge

C m

[I][T][L]

Electric Polarization

P

P = ∂⟨p⟩/∂V  

C m−2

[I][T][L]−2

Absolute Electric Potential relative to point r0  

Theoretical: r0 = ∞  

Practical: R0 = Rearth  

(Earth's radius)

φ ,V

$V = -\frac{W_{\infty r }}{q} = -\frac{1}{q}\int_\infty^r \mathbf{F} \cdot \mathrm{d} \mathbf{r} = -\int_{r_1}^{r_2} \mathbf{E} \cdot \mathrm{d} \mathbf{r}\,\!$

V = J C−1

Electric Potential Difference

ΔφV

$\Delta V = -\frac{\Delta W}{q} = -\frac{1}{q}\int_{r_1}^{r_2} \mathbf{F} \cdot \mathrm{d} \mathbf{r} = -\int_{r_1}^{r_2} \mathbf{E} \cdot \mathrm{d} \mathbf{r} \,\!$

Electric Potential Energy

U

U =  − W  

J

[M][L]2[T]2

Magnetic Quantities

Quantity (Common Name/s)

(Common) Symbol/s

Defining Equation

SI Units

Dimension

Magnetic Field, Field Strength,

Flux Density, Induction Field

B

F = q(v×B)  

T = N A−1 m−1

Magnetic Flux

ΦB

ΦB = ∫SB ⋅ dA  

Wb = T m-2

Relative Permeability

μr

H m−1

Absolute Magnetic Permeability

μ

μ = μrμ0  

H m−1

Magnetic Field Intensity,

(AKA field strength)

H

$\mathbf{H} =\frac{\mathbf{B}}{\mu}\,\!$

Magnetic Dipole Moment

m, μ, Π

m = NIA  

N is the number of turns of conductor

A m2

[I][L]2

Magnetization

M

$\mathbf{M} = \frac{\partial \langle \mathbf{m} \rangle }{\partial V} \,\!$

Self Inductance

L

Two equivalent definitions are in fact possible:

$L=N\frac{\partial \Phi}{\partial I}\,\!$

$L\frac{\partial I}{\partial t}=-NV\,\!$

H = Wb A−1

Mutual Inductance

M

Again two equivalent definitions are in fact possible:

$M_{X}=N\frac{\partial \Phi_Y}{\partial I_X}\,\!$

$M\frac{\partial I_Y}{\partial t}=-NV_X\,\!$

X,Y subscripts refer to two conductors mutually inducing

voltage/ linking magnetic flux though each other

H = Wb A−1

Electric Circuits

Quantity (Common Name/s)

(Common) Symbol/s

Defining Equation

SI Units

Dimension

Electrical Resistance

R  

R = V/I  

Ω = V A−1 = J s C−2

[M][L]2 [T]−3 [I]−2

Resistivity, Scalar

ρ  

$\rho = \frac{RA}{l} \,\!$

Ω m

[M]2 [L]2 [T]−3 [I]−2

Resistivity Temperature Coefficient,

Linear Temperature Dependance

α  

ρ − ρ0 = ρ0α(TT0)  

K−1

[Θ]−1

Terminal Voltage for

Power Supply

Vter  

V = J C−1

[M] [L]2 [T]−3 [I]−1

Load Voltage for Circuit

Vload  

V = J C−1

[M] [L]2 [T]−3 [I]−1

Internal Resistance of

Power Supply

Rint  

$R_\mathrm{int} = \frac{V_\mathrm{ter}}{I} \,\!$

Ω = V A−1 = J s C−2

[M][L]2 [T]−3 [I]−2

Load Resistance of

Circuit

Rext  

$R_\mathrm{ext} = \frac{V_\mathrm{load}}{I} \,\!$

Ω = V A−1 = J s C−2

[M][L]2 [T]−3 [I]−2

Electromotive Force (emf), Voltage across

entire circuit including power supply, external

components and conductors

ℰ  

ℰ = Vter + Vload  

V = J C−1

[M] [L]2 [T]−3 [I]−1

Electrical Conductance

G  

G = 1/R  

S = Ω−1

[T]3 [I]2 [M]−1 [L]−2

Electrical Conductivity, Scalar

σ  

σ = 1/ρ  

Ω−1 m−1

[I]2 [T]3 [M]−2 [L]−2

Electrical Power

P  

P = VI  

W = J s−1

[M] [L]2 [T]−3

References

  • Dynamics and Relativity, J.R. Forshaw, A.G. Smith, Wiley, 2009, ISBN 978 0 470 01460 8
  • Essential Principles of Physics, P.M. Whelan, M.J. Hodgeson, 2nd Edition, 1978, John Murray, ISBN 0 7195 3382 1
  • Encyclopedia of Physics, R.G. Lerner, G.L. Trigg, 2nd Edition, VHC Publishers, Hans Warlimont, Springer, 2005, pp 12-13