Physics equations/Equations

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00-Mathematics for this course
 Measured in radians, $$\theta = s/r$$ defines angle (in radians), where s is arclength and r is radius. The circumference of a circle is $$C_\odot = \,2\pi r$$ and the circle's area is $$A_\odot = \,\pi r^2$$ is its area. The surface area of a sphere is $$A_\bigcirc = 4\pi r^2$$ and sphere's volume is $$V_\bigcirc = \frac{4}{3}\pi r^3$$

A vector can be expressed as, $$\vec A = A_x \, \hat i+ A_y \, \hat j$$, where  $$A_x=A\cos\theta$$, and  $$A_y=A\sin\theta$$ are the x and y components. Alternative notation for the unit vectors $$(\hat i, \hat j)$$ include $$(\hat x, \hat y)$$ and $$(\widehat {e_1}, \widehat {e_2})$$. An important vector is the displacement from the origin, with components are typically written without subscripts: $$\vec r = x\hat x + y\hat y$$. The magnitude (or absolute value or norm) of a vector is is $$A \equiv |\vec A|= \sqrt{A_x^2 + A_y^2} \quad$$, where the angle (or phase), $$\theta$$, obeys $$\tan\theta=y/x$$, or (almost) equivalently, $$\theta = \arctan{(y/x)} \quad$$. As with any function/inverse function pair, the tangent and arctangent are related by $$\tan(\tan^{-1}\mathcal X) = \mathcal X$$ where $$\mathcal X = y/x$$. The arctangent is not a true function because it is multivalued, with $$\tan^{-1}(\tan \theta) = \theta\; or\; \theta+\pi$$. The geometric interpretations of $$\vec A +\vec B =\vec C$$ and $$\vec B = \vec C -\vec A$$ are shown in the figure. Vector addition and subtraction can also be defined through the components: $$\vec A +\vec B =\vec C \Leftrightarrow$$ $$A_x + B_x =C_x$$ AND $$A_y + B_y =C_y$$ 

01-Introduction
 
 * 1 kilometer = .621 miles and 1 MPH = 1 mi/hr ≈ .447 m/s
 * Typically air density is 1.2kg/m3, with pressure 105Pa. The density of water is 1000kg/m3.
 * Earth's mean radius ≈ 6371km, mass ≈ $6 kg$, and gravitational acceleration = g ≈ 9.8m/s2
 * Universal gravitational constant = G ≈ $6.67 m^{3}·kg^{−1}·s^{−2}$
 * Speed of sound ≈ 340m/s and the speed of light = c ≈ 3×108m/s
 * One light-year ≈ 9.5×1015m ≈ 63240AU (Astronomical unit)
 * The electron has charge, e ≈ 1.6 × 10−19C and mass ≈ 9.11 × 10-31kg. 1eV = 1.602 × 10-19J is a unit of energy, defined as the work associated with moving one electron through a potential difference of one volt.
 * 1 amu = 1 u ≈ 1.66 × 10-27 kg is the approximate mass of a proton or neutron.
 * Boltzmann's constant = kB≈ 1.38 × 10-23 J K−1, and the gas constant is R = NAkB≈8.314 J  K−1  mol−1, where NA≈ 6.02 × 1023 is the Avogadro number.
 * $$k_{\mathrm{e}} = \frac{1}{4\pi\varepsilon_0} \,$$≈ 8.987× 109 N·m²·C−2 is a fundamental constant of electricity; also $$ \varepsilon_0 = \frac{1}{ 4\pi k_{\mathrm{e}}  }  \, $$ ≈ 8.854 × 10−12 F·m−1 is the vacuum permittivity or the electric constant.
 * $$ \mu_0 \,$$ = 4π × 10−7 NA ≈ 1.257 × 10−6 N A (magnetic permeability) is the fundamental constant of magnetism: $$\sqrt{\varepsilon_0\mu_0}=1/c$$.
 * $$\hbar $$ = h/(2π) ≈ 1.054×10−34 J·s the reduced Planck constant, and $$a_0 = \frac{\hbar^2}{k_e m_e e^2} $$ ≈ .526 × 10−10 m is the Bohr radius.

02-One dimensional kinematics
 Difference is denoted by $$d\mathcal X$$, $$\delta\mathcal X$$, or the Delta. $$\Delta\mathcal X = \mathcal X_f - \mathcal X_i$$ or $$\mathcal X - \mathcal X_0$$. Average, or mean, is denoted by $$\bar{\mathcal X}=\langle \mathcal X\rangle = \mathcal X_\text{ave}=\Sigma \mathcal X_i\mathcal/N \ \text{or} \ \Sigma \mathcal P_i\mathcal X_i$$, where $$\mathcal N$$ is number and $$\mathcal P_i$$ are probabilities. The average velocity is $$\bar v = \Delta x/\Delta t$$, and the average acceleration is $$\bar a = \Delta v/\Delta t$$, where $$x$$ denotes position. In CALCULUS, instantaneous values  are denoted by v(t)=dx/dt and a=dv/dt=d2x/dt2.

The equations of motion for uniform acceleration are: $$x= x_0 + v_0t+\tfrac 1 2 at^2$$, and, $$v = v_0+at$$. Also, $$v^2 = v_0^2 + 2a\left( x - x_0 \right)$$, and, $$x - x_0   = \tfrac 1 2 (v_0+v)= \bar vt$$. Note that $$\bar v = \tfrac 1 2 (v_0+v)$$ only if the acceleration is uniform. 

03-Two-Dimensional Kinematics
 $$v^2=v_0^2+ 2a_x\Delta x + 2a_y\Delta y$$  ... in advanced notation this becomes  $$\Delta (v^2) = 2\vec a\cdot\Delta\vec\ell$$.

In free fall we often set, ax=0 and  ay= -g. If angle is measured with respect to the x axis:

$$ v_x = v\cos\theta$$     $$ v_y =  v\sin\theta$$     $$ v_{x0} =  v_0\cos\theta_0$$     $$ v_{y0} =  v_0\sin\theta_0$$ The figure shows a Man moving relative to Train with velocity, $$\vec v_{M|T}$$, where the velocity of the train relative to Earth is, $$\vec v_{T|E}$$ is the velocity of the Train relative to Earth. The velocity of the Man relative to Earth is,

$$\underbrace{\vec v_{M|E}}_{50\;km/hr}=\underbrace{\vec v_{M|T}}_{10\;km/hr}+\underbrace{\vec v_{T|E}}_{40\;km/hr}\,$$ If the speeds are relativistic, define u=v/c where c is the speed of light, and this formula must be modified to: $$u_{A|O}= \frac{u_{A|O'}+ u_{O'|O}}{1+ (u_{A|O\,'})(u_{O\,'|O})}$$ 

04-Dynamics: Force and Newton's Laws
 Newton's laws of motion, can be expressed with two equations, $$ m\vec a = \sum\vec F_j  \,$$ and $$\vec F_{ij}=-\vec F_{ji}$$. The second represents the fact that the force that the i-th object exerts one object exerts on the j-th object is equal and opposite the force that the j-th exerts on the i-th object. Three non-fundamental forces are:
 * 1) The normal force, $$N$$, is a contact forces that is perpendicular to the surface,
 * 2) The force of friction, $$f$$, is a contact force that is parallel to the surface.
 * Tension, $$T$$, is often associated with ropes and strings. If the rope has sufficiently low weight and of all external forces act at the two ends, then this tension is distributed uniformly along the rope.
 * 1) The fourth force is fundamental: Weight equals $$mg$$, and is the force of gravity acting on an object of mass, $$m$$. At Earth's surface, $$g\approx9.8m/s^2$$.

The x and y components of the three forces of tension on the small grey circle where the three "massless" ropes meet are:
 * $$T_{1x}=-T_1\cos\theta_1 $$,          $$ T_{1y}=T_1\sin\theta_1$$
 * $$T_{2x}=0 $$,                                   $$T_{2y}=-mg$$
 * $$T_{3x}=T_3\cos\theta_3 $$,             $$T_{3y}=T_3\sin\theta_3$$



05-Friction, Drag, and Elasticity
 
 * $$f_k=\mu_k N$$ is an approximation for the force friction when an object is sliding on a surface, where μk ("mew-sub-k") is the kinetic coefficient of friction, and N is the normal force.
 * $$f_s\le \mu_sN$$ approximates the maximum possible friction (called static friction) that can occur before the object begins to slide. Usually μs > μk. Also,  air drag  often depends on speed, an effect this model fails to capture.

06-Uniform Circular Motion and Gravitation

 * $$2\pi\;rad=360\;deg=1\;rev$$ relates the radian, degree, and revolution.


 * $$f = \frac{\#\,\text{revs}}{\#\,\text{secs}}$$ is the number of revolutions per second, called frequency.


 * $$T = \frac{\#\,\text{secs}}{\#\,\text{revs}}$$ is the number of seconds per revolution, called period. Obviously $$fT = 1$$.


 * $$\omega = \frac{\Delta\theta}{\Delta t}$$ is called angular frequency (ω is called omega, and &theta; is measured in radians). Obviously $$\omega T = 2\pi$$


 * $$a=\frac{v^2}{r}=\omega v =\omega^2 r$$ is the acceleration of uniform circular motion, where v is speed, and r is radius.
 * $$v=\omega r =2\pi r/T$$, where T is period.


 * $$F = G \frac{mM}{r^2}= mg^*$$ is the force of gravity between two objects, where the universal constant of gravity is G ≈ 6.674 × 10-11 m3·kg−1·s−2.



07-Work and Energy
 
 * $$KE = \frac 1 2 m v^2\,$$ is kinetic energy, where m is mass and v is speed..
 * $$U_g = mgy$$ is gravitational potential energy,where y is height, and $$g = 9.80\;\frac{m}{s^2}$$ is the gravitational acceleration at Earth's surface.
 * $$U_s = \frac 1 2 k_s x^2$$ is the potential energy stored in a spring with spring constant $$k_s$$.
 * $$\sum KE_f + \sum PE_f = \sum KE_i + \sum PE_i -Q$$ relates the final energy to the initial energy. If energy is lost to heat or other nonconservative force, then Q>0.
 * $$W = F \ell\cos\theta=\vec F\cdot\vec\ell$$ (measured in Joules) is the work done by a force $$F$$ as it moves an object a distance $$\ell$$. The angle between the force and the displacement is &theta;.
 * $$\sum \vec F\cdot\Delta\ell$$ describes the work if the force is not uniform. The steps, $$\Delta\vec\ell$$, taken by the particle are assumed small enough that the force is approximately uniform over the small step.  If force and displacement are parallel, then the work becomes the area under a curve of F(x) versus x.
 * $$P=\frac{\vec F \cdot \vec\Delta \ell}{\Delta t}=\vec F\cdot\vec v$$ is the power (measured in Watts) is the rate at which work is done. (v is velocity.)

08-Linear Momentum and Collisions
<section begin=08-Linear_Momentum_and_Collisions/> <section end=08-Linear_Momentum_and_Collisions/>
 * $$ \vec p = m\vec v$$ is momentum, where m is mass and $$ \vec v$$ is velocity. The net momemtum is conserved if all forces between a system of particles are internal (i.e., come equal and opposite pairs):
 * $$\sum \vec p_f = \sum \vec p_i$$.
 * $$\bar F\Delta t = \Delta p$$ is the impulse, or change in momentum associated with a brief force acting over a time interval $$\Delta t$$. (Strictly speaking, $$\bar F$$ is a time-averaged force defined by integrating over the time interval.)

09-Statics and Torque
<section begin=09-Statics_and_Torque/>
 * $$\tau = rF\sin\theta,\!$$ is the torque caused by a force, F, exerted at a distance ,r, from the axis. The angle between r and F is &theta;.

The for torque is the  (N·m). It would be inadvisable to call this a Joule, even though a Joule is also a (N·m). The symbol for torque is typically τ, the Greek letter tau. When it is called moment, it is commonly denoted M. The lever arm is defined as either r, or r⊥. Labeling r as the lever arm allows moment arm to be reserved for r⊥. <section end=09-Statics_and_Torque/>

10-Rotational Motion and Angular Momentum
<section begin=10-Rotational_Motion_and_Angular Momentum/>

<section end=10-Rotational_Motion_and_Angular Momentum/>

11-Fluid statics
<section begin=11-Fluid_statics/> Pressure versus Depth: A fluid's pressure is F/A where F is force and A is a (flat) area. The pressure at depth, $$h$$ below the surface is the weight (per area) of the fluid above that point. As shown in the figure, this implies:


 * $$ P = P_0 + \rho g h $$

where $$P_0$$ is the pressure at the top surface, $$h$$ is the depth, and $$\rho$$ is the mass density of the fluid. In many cases, only the difference between two pressures appears in the final answer to a question, and in such cases it is permissible to set the pressure at the top surface of the fluid equal to zero. In many applications, it is possible to artificially set $$P_0$$ equal to zero, for example at atmospheric pressure. The resulting pressure is called the gauge pressure, for $$ P_{gauge} = \rho gh $$ below the surface of a body of water.

Buoyancy and Archimedes' principle Pascal's principle does not hold if two fluids are separated by a seal that prohibits fluid flow (as in the case of the piston of an internal combustion engine). Suppose the upper and lower fluids shown in the figure are not sealed, so that a fluid of mass density $$\rho_{flu}$$ comes to equilibrium above and below an object. Let the object have a mass density of $$\rho_{obj}$$ and a volume of $$A\Delta h$$, as shown in the figure. The net (bottom minus top) force on the object due to the fluid is called the buoyant force:


 * $$\rm{buoyant}\;\rm{force}=(A\Delta h )(\rho_{flu})g\,$$,

and is directed upward. The volume in this formula, AΔh, is called the volume of the displaced fluid, since placing the volume into a fluid at that location requires the removal of that amount of fluid. Archimedes principle states:


 * A body wholly or partially submerged in a fluid is buoyed up by a force equal to the weight of the displaced fluid.

Note that if $$\rho_{obj}=\rho_{flu}$$, the buoyant force exactly cancels the force of gravity. A fluid element within a stationary fluid will remain stationary. But if the two densities are not equal, a third force (in addition to weight and the buoyant force) is required to hold the object at that depth. If an object is floating or partially submerged, the volume of the displaced fluid equals the volume of that portion of the object which is below the waterline. <section end=11-Fluid_statics/>

12-Fluid dynamics
<section begin=12-Fluid_dynamics/> <section end=12-Fluid_dynamics/>
 * $$\frac{\Delta V}{ \Delta t } =\dot V=Av = Q$$ the volume flow for incompressible fluid flow if viscosity and turbulence are both neglected. The average velocity is $$v$$ and $$A$$ is the cross sectional area of the pipe.  As shown in the figure, $$v_1A_1=v_2A_2$$ because $$Av$$ is constant along the developed flow.  To see this, note that the volume of pipe is $$\Delta V=A\Delta x$$ along a distance $$\Delta x$$. And, $$v = \Delta x / \Delta t$$ is the volume of fluid that passes a given point in the pipe during a time $$\Delta t$$.
 * $$P_1 + \rho g y_1 + \frac{1}{2}\rho v_1^2 = P_2 + \rho g y_2 + \frac{1}{2}\rho v_2^2$$ is Bernoulli's equation, where $$P$$ is pressure, $$\rho$$ is density, and $$y$$ is height. This holds for inviscid flow.

13-Temperature, Kinetic Theory, and Gas Laws
<section begin=13-Temperature,_Kinetic Theory,_and_Gas_Laws/> <section end=13-Temperature,_Kinetic Theory,_and_Gas_Laws/>
 * $$T_C=T_K-273.15$$ converts from Celsius to Kelvins, and $$T_F=\frac 9 5 T_C+32$$ converts from Celsius to Fahrenheit.
 * $$PV=nRT=Nk_BT$$ is the ideal gas law, where P is pressure, V is volume, n is the number of moles and N is the number of atoms or molecules. Temperature must be measured on an absolute scale (e.g. Kelvins).
 * NAkB=R where NA= 6.02 × 1023 is the Avogadro number. Boltzmann's constant can also be written in eV and Kelvins: kB ≈8.6 × 10-5 eV/deg.
 * $$\frac 3 2 k_B T =\frac 1 2 mv_{rms}^2$$ is the average translational kinetic energy per "atom" of a 3-dimensional ideal gas.
 * $$v_{rms}=\sqrt{\frac{3k_BT}{m}}=\sqrt{\overline{v^2}}$$ is the root-mean-square speed of atoms in an ideal gas.
 * $$E = \frac{\varpi}{2}Nk_BT$$ is the total energy of an ideal gas, where $$\varpi=3\;$$

14-Heat and Heat Transfer
<section begin=14-Heat_and_Heat_Transfer/> Here it is convenient to define heat as energy that passes between two objects of different temperature $$Q$$ The SI unit is the Joule. The rate of heat trasfer, $$\Delta Q/\Delta t$$ or $$\dot Q$$ is "power": 1 Watt = 1 W = 1J/s <section end=14-Heat_and_Heat_Transfer/>
 * $$Q = mc_S\Delta T$$ is the heat required to change the temperature of a substance of mass, m. The change in temperature is &Delta;T.  The specific heat, cS, depends on the substance (and to some extent, its temperature and other factors such as pressure).  Heat is the transfer of energy, usually from a hotter object to a colder one.  The units of specfic heat are energy/mass/degree, or J/(kg-degree).
 * $$Q = mL$$ is the heat required to change the phase of a a mass, m, of a substance (with no change in temperature). The latent heat, L, depends not only on the substance, but on the nature of the phase change for any given substance.  LF is called the latent heat of fusion, and refers to the melting or freezing of the substance.  LV is called the latent heat of vaporization, and refers to evaporation or condensation of a substance.
 * $$\dot Q= \frac{k_cA}{d}\Delta T$$ is rate of heat transfer for a material of area, A. The difference in temperature between two sides separated by a distance, d, is $$\Delta T$$. The thermal conductivity, kc, is a property of the substance used to insulate, or subdue, the flow of heat.
 * $$\dot Q= \sigma A\epsilon T^{4}$$ is the power radiated by a surface of area, A, at a temperature, T, measured on an absolute scale such as Kelvins. The emissivity, $$0\le\epsilon\le 1$$, is 1 for a black body, and 0 for a perfectly reflecting surface.  The Stefan-Boltzmann constant is $$\sigma\approx 5.67 \times 10^{-8}\, \mathrm{J\, s^{-1}m^{-2}K^{-4}}$$.

15-Thermodynamics
<section begin=15-Thermodynamics/> A point on a PV diagram define's the system's pressure (P) and volume (V). Energy (E) and pressure (P) can be deduced from equations of state: E=E(V,P) and T=T(V,P). If the piston moves, or if heat is added or taken from the substance, energy (in the form of work and/or heat) is added or subtracted. If the path returns to its original point on the PV-diagram (e.g., 12341 along the rectantular path shown), and if the process is quasistatic, all state variables (P, V, E, T) return to their original values, and the final system is indistinguishable from its original state.
 * Pressure (P), Energy (E), Volume (V), and Temperature (T) are state variables (state functionscalled state functions). The number of particles (N) can also be viewed as a state variable.
 * Work (W), Heat (Q) are not state variables.
 * $$ S (V,T)= \frac{3 Nk_B}{2}\ln T+ Nk_B\ln V + constant$$, is the entropy of an ideal, monatomic gas. The constant is arbitrary only in classical (non-quantum) thermodynamics. Since it is a function of state variables, entropy is also a state function.

The net work done per cycle is area enclosed by the loop. This work equals the net heat flow into the system, $$Q_{in} - Q_{out} $$ (valid only for closed loops).

Remember: Area "under" is the work associated with a path; Area "inside" is the total work per cycle.


 * $$\Delta W=-F\Delta x= ( -P\cdot\mathrm{Area} ) \left( \frac{\Delta V}{\mathrm{Area}} \right) = -P\Delta V$$ is the work done on a system of pressure P by a piston of voulume V. If ΔV>0 the substance is expanding as it exerts an outward force, so that ΔW<0 and the substance is doing work on the universe; ΔW>0 whenever the universe is doing work on the system.
 * $$\Delta Q$$ is the amount of heat (energy) that flows into a system. It is positive if the system is placed in a heat bath of higher temperature. If this process is reversible, then the heat bath is at an infinitesimally higher temperature and a finite &Delta;Q takes an infinite amount of time.
 * $$\Delta E=\Delta Q-P\Delta V$$ is the change in energy (First Law of Thermodynamics).

CALCULUS: $$ \oint P \ dV = Q_{in} - Q_{out}$$.


 * In an isothermal expansion (contraction), temperature, T, is constant. Hence P=nRT/V and substitution yields,
 * $$\int_{Vi}^{Vf}PdV=\int_{Vi}^{Vf}nRT\frac{dV}{V}=nRT\int_{Vi}^{Vf}\frac{dV}{V}=nRT\ln\frac{V_f}{V_i}$$

<section end=15-Thermodynamics/>

16-Oscillatory Motion and Waves
<section begin=16-Oscillatory_Motion_and_Waves/>
 * $$ x = x_0\cos{  \frac{2\pi t}{T_0}   }$$ describes oscillatory motion with period $$T_0$$ (here we use the zero-subscript to denote constants that do not vary with time).
 * $$ x(t) = x_0\cos\left(\omega_0 t - \varphi\right)$$. For example, $$\cos\left(\omega_0 t - \varphi\right)= \sin\omega_0 t$$.
 * $$\omega_0=\sqrt{\frac{k_s}{m}}=\frac{2\pi}{T}$$ for a mass-spring system with mass, m, and spring constant, ks.
 * $$\omega_0=\sqrt{\frac{g}{L}}=\frac{2\pi}{T}$$ for a low amplitude pendulum of length, L, in a gravitational field, g.
 * $$PE=\frac 1 2 k_s x^2$$ is the potential energy of a mass spring system.

Let $$ x(t) = x_0\cos\left(\omega_0 t - \varphi\right) =$$ describe position: =a_0\cos\left(\omega_0 t + ...\right)$$, where $$a_0=\omega_0 v_0=\omega_0^2 x_0$$, is maximum acceleration. <section end=16-Oscillatory_Motion_and_Waves/>
 * $$v(t) = dx/dt = -\omega_0 x_0\sin\left(\omega_0 t - \varphi\right)=v_0\cos\left(\omega_0 t + ...\right)$$, where $$v_0=\omega_0 x_0$$ is maximum velocity.
 * $$ a(t) = dv/dt =-\omega_0 v_0\cos\left(\omega_0 t - \varphi\right)
 * $$F_0=m a_0$$, relates maximum force to maximum acceleration.
 * $$E=\frac 1 2 mv_0^2=\frac 1 2 k_s x_0^2$$ is the total energy.
 * CALCULUS: x(t) obeys the linear homogeneous differential equation (ODE), $$\frac{d^2x}{dt^2} = -\omega_0^2 x(t)$$
 * $$f\lambda = v_p$$ relates the frequency, f, wavelength, &lambda;,and the the phase speed, vp of the wave (also written as vw)   This phase speed is the speed of individual crests, which for sound and light waves also equals the speed at which a wave packet travels.
 * $$L = \frac{n\lambda_n}{2}$$ describes the n-th normal mode vibrating wave on a string that is fixed at both ends (i.e. has a node at both ends). The mode number, n = 1, 2, 3,..., as shown in the figure.
 * Beat frequency: The frequency of beats heard if two closely space frequencies, $$f_1$$ and $$f_2$$, are played is $$\Delta f = |f_2-f_1|$$.
 * Musical acoustics: Frequency ratios of 2/1, 3/2, 4/3, 5/3, 5/4, 6/5, 8/5 are called the (just) "octave", "fifth",    "fourth", "major-sixth", "major-third", "minor-third", and "minor-sixth",  respectively.

17-Physics of Hearing
<section begin=17-Physics_of_Hearing/> <section end=17-Physics_of_Hearing/>
 * $$v_s =\sqrt{  \frac{T}{273}    }\cdot 331 \text{m/s}$$ is the the approximate speed near Earth's surface, where the temperature, T, is measured in Kelvins.  A theoretical calculation is $$v_s=\sqrt{\frac{\gamma k_B T}{m}}$$ where $$\gamma =\frac{\varpi+2}{\varpi}$$ for a semi-classical gas with $$\varpi$$ degrees of freedom. For a diatomic gas such as Nitrogen, &gamma; = 1.4.
 * $$v_s =\sqrt{  \frac{F}{\mu}    }$$ is the speed of a wave in a stretched string if $$F$$ is the tension and $$\mu$$ is the linear mass density (kilograms per meter).

18-Electric charge and field
<section begin=18-Electric_charge_and_field/>
 * $$F=k_{\mathrm{e}} \frac{qQ}{r^2} = \frac{1}{ 4\pi \epsilon_0  } \frac{qQ}{r^2}\,$$ is Coulomb's law for the force between two charged particles separated by a distance r: ke≈8.987×109N·m²·C−2, and ε0≈8.854×10−12 F·m−1.
 * $$\vec F=q\vec E$$ is the electric force on a "test charge", q, where $$E =k_{\mathrm{e}} \frac{Q}{r^2} \,$$ is the magnitude of the electric field situated a distance r from a charge, Q.

Consider a collection of $$N$$ particles of charge $$Q_i$$, located at points $$\vec r_i$$ (called source points), the electric field at $$\vec r $$ (called the field point) is: =\frac{1}{4\pi \varepsilon_0}\sum_{i=1}^N \frac{\widehat\mathcal{R}_i Q_i}{|\mathcal{\vec R}_i |^2} = \frac{1}{4\pi \varepsilon_0}\sum_{i=1}^N \frac{\vec\mathcal{R}_i Q_i}{|\mathcal{\vec R}_i |^3} $$ is the electric field at the field point, $$\vec r $$, due to point charges at the source points,$$\vec r_i$$, and $$ \vec\mathcal R_i = \vec r - \vec r_i ,$$ points from source points  to the field point.
 * $$ \vec{E}(\vec r)

 CALCULUS  supplement:

$$ \vec{E}(\vec r)= k_e\int\frac{\hat\mathcal R dQ}{\mathcal R^2}$$ is the electric field due to distributed charge, where $$ dQ\rightarrow\lambda d\ell\rightarrow \sigma dA\rightarrow\rho dV\;$$, and  $$(\lambda, \sigma, \rho)$$ denote linear, surface, and volume density (or charge density), respectively.

Cartesian coordinates (x, y, z). Volume element: $$dV=dxdydz$$. Line element:$$d\vec\ell =\hat x dx+\hat y dy+\hat z dz$$. Three basic area elements: $$\hat ndA = $$$$\hat z dxdy$$, or,$$ \hat x dydz $$, or,$$\hat y dzdx$$.

Cylindrical coordinates (&rho;, &phi;, z): Volume element: $$dV =\rho\,dr\,d\varphi \,dz$$. Line element:$$d\vec\ell =\hat\varphi rd\varphi+\hat r dr+\hat zdz$$. Basic area elements: $$\hat ndA = \rho\,d\varphi\,dz\,\hat \rho$$ (side), and, $$\rho\,d\rho\,d\varphi\,\hat z$$ (top end).

Spherical coordinates (r, &theta;, &phi;): Volume element: $$dV = r^2\,dr\,\sin\theta\,d\theta\,d\varphi \rightarrow 4\pi r^2dr$$ (if symmetry holds). Line element:$$ d\vec\ell= \hat r \,dr+ \hat\theta\, r\, d\theta +   \hat \varphi\, r\, \sin{\theta} \, d\varphi$$. Basic area element of a sphere: $$\hat r dA = \hat r\,r^2 d\Omega$$, where d&Omega; is a solid angle. <section end=18-Electric_charge_and_field/>

19-Electric Potential and Electric Field
<section begin=19-Electric_Potential_and_Electric_Field/>
 * $$U=qV$$ is the potential energy of a particle of charge, q, in the presence of an electric potential V.
 * $$\Delta V = -E \ell\cos\theta=\vec E\cdot\vec\ell$$ (measured in Volts) is the variation in electric potential as one moves through an electric field $$E$$. The angle between the field and the displacement is &theta;.  The electric potential, V, decreases as one moves parallel to the electric field.
 * $$\Delta V = -\sum \vec E\cdot\Delta\ell$$ describes the electric potential if the field is not uniform.
 * $$V(\vec r) = k\sum\frac{Q_j}{\mathcal R_j}$$ due to a set of charges $$Q_j$$ at $$\vec r_j$$ where $$\vec\mathcal R_j = \vec r - \vec r_j$$.


 * $$Q=CV$$ is the (equal and opposite) charge on the two terminals of a capacitor of capicitance, C, that has a voltage drop, V, across the two terminals.
 * $$C=\varepsilon A/d$$ is the capacitance of a parallel plate capacitor with surface area, A, and plate separation, d. This formula is valid only in the limit that d2/A vanishes.  If a dielectric is between the plates, then ε>ε0≈ 8.85 × 10−12 due to shielding of the applied electric field by dielectric polarization effects.
 * $$U=\frac 1 2 QV = \frac 1 2 CV^2 = \frac{Q^2}{2C} $$ is the energy stored in a capacitor.
 * $$u=\frac{\varepsilon}{2}E^2$$ is the energy density (energy per unit volume, or Joules per cubic meter) of an electric field.

CALCULUS supplement


 * $$ \int_\vec p^\vec q \vec\nabla f\cdot d\vec\ell =  f (\vec{q}\,)- f(\vec{p}\,)   $$ is the gradient theorem.


 * $$ \int_{\Sigma} \vec\nabla \times \vec F \cdot \vec{dA} = \oint_{\partial\Sigma}\vec F\cdot d\hat\ell$$ is Stokes' theorem

\oint_{\partial \Omega} \vec F \cdot d\vec A $$ is the divergence theorem
 * $$\int_{\Omega} \vec\nabla \cdot \vec F \;dV=

Here, &Omega; is a (3-dimensional) volume and &part;&Omega; is the boundary of the volume, which is a (two-dimensional) surface. Also a surface is &Sigma;, which, if open, has the boundary &part;&Sigma;, which is a (one-dimensional) curve.


 * $$ V(\vec b) -V(\vec a)=-\int_{\vec a}^{\vec b} \vec E\cdot d\ell$$ in the limit that the Riemann sum becomes an integral.
 * $$\vec E = -\vec\nabla V$$ where $$\vec\nabla $$ $$= \hat x\partial/\partial x +\hat y\partial/\partial y +\hat z\partial/\partial z $$ is the del operator.


 * $$ \varepsilon_0\int \vec E \cdot \vec{dA} = Q_{encl}$$ is Gauss's law for the surface integral of the electric field over any closed surface, and $$Q_{encl}$$ is the total charge inside that surface.
 * $$ \int \vec D \cdot \vec{dA} = Q_{free}$$ is a useful variant if the medium is dielectric.  D=εE is the electric displacement field.  The permittivity, ε = (1+χ)ε0, where  ε0≈ 8.85 × 10−12, and the electric susceptibility, χ, represents the degree to which the medium can be polarized by an electric field.  The free charge, Qfree, represents all charges except those represented by the susceptibility, χ.

<section end=19-Electric_Potential_and_Electric_Field/>

20-Electric Current, Resistance, and Ohm's Law
<section begin=20-Electric_Current,_Resistance,_and_Ohm's_Law/> <section end=20-Electric_Current,_Resistance,_and_Ohm's_Law/>
 * $$I = \frac{\mathrm{d}Q}{\mathrm{d}t} \ $$ defines the electric current as the rate at which charge flows past a given point on a wire. The direction of the current matches the flow of positive charge (which  is opposite the flow of electrons if electrons are the carriers.)
 * $$V = I R $$ is Ohm's Law relating current, I, and resistance, R, to the difference in voltage, V, between the terminals.  The resistance, R, is positive in virtually all cases, and if R > 0, the current flows from larger to smaller voltage.  Any device or substance that obeys this linear relation between I and V is called ohmic.
 * $$I=nqAv_{drift}$$ relates the density (n), the charge(q), and the average drift velocity (vdrift) of the carriers. The area (A) is measured by imagining a cut across the wire oriented such that the drift velocity is perpendicular to the surface of the (imaginary) cut.
 * $$R=\frac{\rho L}{A} \ $$ expresses the resistance of a sample of ohmic material with a length (L) and area (A). The 'resistivity', &rho; ("row"), is an intensive property of matter.
 * Power is energy/time, measured in joules/second or J/s. Often called P (never p).  It is measured in watts (W)
 * Current is charge/time, measured in coulombs/second or C/s. Often called I or i.  It is measured in amps or ampheres (A)
 * Electric potential (or voltage) is energy/charge, measured in joules/coulomb or J/C. Often called V (sometimes E, emf, $$\mathcal E$$).  It is measured in volts (V)
 * Resistance is voltage/current, measured in volts/amp or V/A. Often called R (sometimes r, Z) It is measured in Ohms (Ω).
 * $$P = IV = I^2R=\frac{V^2}{R}$$ is the power dissipated as current flows through a resistor

21-Circuits, Bioelectricity, and DC Instruments
<section begin=21-Circuits,_Bioelectricity,_and_DC_Instruments/>
 * $$\sum_{k=1}^n {I}_k = 0$$ and $$\sum_{k=1}^n V_k = 0$$ are Kirchoff's Laws
 * $$V_{\rm out}=\frac{R_2}{R_1+R_2}V_{\rm in}$$ for the voltage divider shown.
 * Simple RC circuit The figure to the right depicts a capacitor being charged by an ideal voltage source. If, at t=0, the switch is thrown to the other side, the capacitor will discharge, with the  voltage, V, undergoing exponential decay:

V(t)=V_0 e^{-\frac{t}{RC}} \ , $$

where V0 is the capacitor voltage at time t = 0 (when the switch was closed). The time required for the voltage to fall to $$\frac{V_0}{e}\approx .37V_0 $$ is called the RC time constant and is given by


 * $$ \tau = RC \ . $$

<section end=21-Circuits,_Bioelectricity,_and_DC_Instruments/>

22-Magnetism
<section begin=22-Magnetism/>
 * Defining magnetic force and field without calculus:Manoderecha.svg
 * 1)   $$B=\frac{\mu_0 I}{2\pi r}$$ is the magnetic field at a distance r from an infinitely long wire carrying a current, where μ0 = 4π × 10−7 N A. This field points azimuthally around the wire in a direction defined by the right hand rule.  Application of the force law on a current element, we have
 * 2)   $$F=\frac{\mu_0 I_1 I_2\,\ell}{2\pi r}$$ is the force between two long wires of length $$\ell$$ separated by a short distance $$r<<\ell$$.  The currents are I1 and I2, with the force being attractive if the currents are flowing in the same direction.

Cyclotron motion: For a particle moving perpendicular to B, we have cyclotron motion. Recall that for uniform circular motion, the acceleration is a=v2/r, where r is the radius. Since sin &theta; =1, Newton's second law of motion (F=ma) yields,


 * $$ma=\frac{mv^2}{r}=qvB$$

Since, sin &theta; =0, for motion parallel to a magnetic field, particles in a uniform magnetic field move in spirals at a radius which is determined by the perpendicular component of the velocity:


 * $$r =\frac{mv_\perp}{qB}$$

Hall effect: The Hall effect occurs when the magnetic field, velocity, and electric field are mutually perpendicular. In this case, the electric and magnetic forces are aligned, and can cancel if qE=qvB (since sinθ = 1). Since both terms are porportional to charge, q, the appropriate ratio of electric to magnetic field for null net force depends only on velocity:


 * $$E = vB = \frac{\mathrm{emf}}{\ell}$$,

where we have used the fact that voltage (i.e. emf or potential) is related to the electric field and a displacement parallel to that field: ΔV = -E Δs cosθ

CALCULUS supplement:
 * $$\vec B=\oint\frac{\mu_0}{4\pi}\frac{I d\vec{\ell} \times \hat r}{|r|^2}$$ and the volume integral $$\int\frac{\mu_0}{4\pi}\frac{\vec J \times \hat r}{|r|^2} d\tau'$$, where $$\vec J$$ is current density.
 * $$\oint \vec B \cdot d\vec\ell = \mu_0 I_{encl}$$ is Ampere's law relating a closed integral involving magnetic field to the total current enclosed by that path.

<section end=22-Magnetism/>

23-Electromagnetic Induction, AC Circuits, and Electrical Technologies
<section begin=23-Electromagnetic_Induction,_AC_Circuits,_and_Electrical_Technologies/> <section end=23-Electromagnetic_Induction,_AC_Circuits,_and_Electrical_Technologies/>
 * $$\vec E = \vec v \times \vec B$$ is a consequence of the magnetic force law as seen in the reference frame of a moving charged object, where E is the electric field perceived by an observer moving at velocity v in the presence of a magnetic vield, B.  Also written as, E = vBsin&theta;, this can be used to derive Faraday's law of induction. (Here, &theta; is the angle between the velocity and the magnetic field.)
 * $$\Phi = \vec A\cdot\vec B = AB\cos\theta$$ is the magnetic flux, where &theta; is the angle between the magnetic field and the normal to a surface of area, A.
 * $$emf=-N\frac{\Delta \Phi}{\Delta t}$$ is Faraday's law where t is time and N is the number of turns. The minus sign reminds us that the emf, or electromotive force, acts as a "voltage" that opposes the change in the magnetic field or flux.

24-Electromagnetic Waves
<section begin=24-Electromagnetic_Waves/> Maxwell's equations hold for all volumes and closed surfaces. In vacuum, electromagnetic waves travel at the speed, $$c = \frac{1}{\sqrt{\epsilon_0\mu_0}}$$. <section end=24-Electromagnetic_Waves/>
 * $$\epsilon_0 \partial\vec E/\partial t$$ is called the displacement current because it replaces the current density when using Ampère's circuital law to calculate the line integral of the magnetic field around a closed loop.

25-Geometric Optics
<section begin=25-Geometric_Optics/> $$\frac{1}{S_1} + \frac{1}{S_2} = \frac{1}{f} $$ relates the focal length f of the lens, the image distance S1, and the object distance S2. The figure depicts the situation for which (S1, S2, f) are all positive: (1)The lens is converging (convex); (2) The real image is to the right of the lens; and (3) the object is to the left of the lens. If the lens is diverging (concave), then f < 0. If the image is to the left of the lens (virtual image), then S2 < 0. <section end=25-Geometric_Optics/>

===26-Vision and Optical Instruments===<section begin=26-Vision_and_Optical_Instruments/>*foo<section end=26-Vision_and_Optical_Instruments/>

27-Wave Optics
<section begin=27-Wave_Optics/>
 * $$S\sin\theta = n\lambda$$ where $$n = 1, 2, 3, 4...$$ describes the constructive interference associated with two slits in the Fraunhoffer (far field) approximation.
 * $$\cos\left(\omega_1t\right)+\cos\left(\omega_2t\right)=A(t)\cos\left(\bar\omega t\right)$$ where $$\bar\omega$$ is the high frequency carrier and $$A(t)=2\cos\left(\frac{\Delta\omega}{2}t\right)$$ is the slowly varying envelope. Here,
 * $$\bar\omega=\frac{\omega_1+\omega_2}{2}$$ and $$\Delta\omega=\omega_2-\omega_1$$. Consequently, the beat frequency heard when two tones of frequency $$f_1$$ and $$f_2$$ is $$\Delta f = f_2-f_1$$.

cos \left(  k\ell_1   -  \omega t  \right)+    cos  \left(   k\ell_2   -   \omega t   \right) =2cos\left(k\Delta\ell\right)\cos(\omega t -\phi) $$ models the addition of two waves of equal amplitude but different path length, $$\Delta\ell=\ell_2-\ell_1$$. <section end=27-Wave_Optics/>

MassRadiusDistanceEarthSunMoon
<section begin=MassRadiusDistanceEarthSunMoon/> <section end=MassRadiusDistanceEarthSunMoon/>
 * Earth's Radius: R⊕ ≈ 6.37x106m
 * Earth's Mass: M⊕ ≈ 5.97×1024kg
 * Solar and Lunar radius and mass:
 * Solar radius and mass: R☉≈110R⊕ and M☉ ≈ 330,000M⊕.
 * Lunar radius and mass: RL ≈ 0.273R⊕ and ML ≈ 0.0123M⊕
 * Earth-moon distance ≈ 60R⊕
 * Earth-Sun distance = 1AU ≈ 1.496x1011m ≈ 23481R⊕
 * One light-year ≈ 9.5×1015 m = 63240 AU
 * One parsec ≈ 3.26 light-years

KeplerNewtonMassPeriodDistanceNorm
<section begin=KeplerNewtonMassPeriodDistanceNorm/> <section end=KeplerNewtonMassPeriodDistanceNorm/>
 * $$a_\mathrm{AU}^3=\tilde M_\mathrm{net}P_\mathrm{year}^2$$, where P is the period of orbit in years, and a is the semi-major axis measured in AU. The net mass, $$\tilde M_\mathrm{net}$$, is the sum of the mass of both bodies, and is normalized to the mass of the Sun.  For a planet of mass, $$m$$, orbiting a star of much larger mass, $$M>>m$$, the normalized net mass is $$\tilde M_\mathrm{net}=\,$$$$(M+m)/M_\odot\approx\,$$$$M/M_\odot$$.  The mass of the Sun, $$M_\odot$$, is  1.99×1030 kilograms. If $$M_\odot =2$$ for some object, then that object is twice as massive as the Sun. One year is 3.15×107 seconds.

AstrParallax
<section begin=AstrParallax/> <section end=AstrParallax/>
 * $$D_\mathrm{parsec}=\frac{b_\mathrm{AU}}{\theta_\mathrm{arcsec}}$$, where D is the distance to the object in parsecs, θ is the parallax angle in arcseconds, and b is the baseline in AU; b=1 for observations taken from Earth. One degree is 60 arcminutes and one arcminute is 60 arseconds.  One AU ≈ 1.5x1011 meters, and one parsec ≈ 3.26 light-years, and one light-year ≈ 9.5×1015 meters.

AstrInverseSquare
<section begin=AstrInverseSquare/> <section end=AstrInverseSquare/>
 * $$4\pi \tilde I=\frac{\tilde L}{D^2}$$ is a "normalized intensity", closely related to relative magnitude, that allows students to combine equations and solve problems without resorting to the logarithmic magnitude scale. If the distance to the stellar object, D, is measured in parsecs, it is the power per square parsec that enters a telescope on Earth.  The luminosity, $$\tilde L$$, (in solar units) is a measure of the absolute magnitude. In general, $$\mbox{Intensity} \ \propto \ \frac{1}{\mbox{distance}^2} \, $$ is the inverse-square law.

PhotonsWavesParticles
<section begin=PhotonsWavesParticles/>

<section end=PhotonsWavesParticles/>
 * $$E=hf=hc/\lambda$$ is the energy of a photon, where f is frequency and h ≈6.6×10-34m2kg/s is Plank's constant, and c ≈3×108m/s is the speed of light.  Also, E= ℏ &omega; where ℏ ≈1.05×10m2kg/s and &omega; =2π f.
 * $$f \lambda=c$$ relates frequency, wavelength, and the speed (or phase velocity). Using wavenumber, k =2π/λ, this can also be represented as &omega; =ck.

AstrBlackbody
<section begin=AstrBlackbody/>
 * $$\lambda_\text{max} T_K = .003\text{nm} $$ is Wein's law that relates the peak emission wavelength, λmax, of a black body to temperature, T measured in Kelvins.  Peak wavelength, λmax, is measured in nanometers (1nm=10-9m).  If temperature is measured in units normalized to the Sun's temperature, $$T_\odot=5778K$$, then
 * $$\lambda_\text{max} \tilde T = 502\text{nm} $$ where $$\tilde T=T/T_\odot$$ is the temperature normalized to the Sun's temperature.

The Stefan-Boltzmann law is usually written as P=σAT4, where A is surface area, T is temperature (in Kelvins), and σ is the Stefan-Boltzmann constant. The power, P, can be written as normalized luminosity, $$\tilde L = P/L_\odot$$, where L☉ =3.85×1026W is the power output (or luminosity) of the Sun. In these normalized units, the Stefan-Boltzmann law is: <section end=AstrBlackbody/>
 * $$\tilde L=\tilde R^2\tilde T^4$$, where $$\tilde R=R/R_\odot$$ is the radius and temperature normalized to the Sun's radius and $$\tilde T=T/T_\odot$$ is the temperature normalized to the Sun's temperature.

Hidden chapters from openstax Physics
===28-Special Relativity=== <section begin=28-Special_Relativity/> <section end=28-Special_Relativity/>
 * foo

29-Introduction to Quantum Physics
<section begin=29-Introduction_to_Quantum_Physics/> <section end=29-Introduction_to_Quantum_Physics/>
 * foo

30-Atomic Physics
<section begin=30-Atomic_Physics/> <section end=30-Atomic_Physics/>
 * foo

31-Radioactivity and Nuclear Physics
<section begin=31-Radioactivity_and_Nuclear_Physics/> <section end=31-Radioactivity_and_Nuclear_Physics/>
 * foo

32-Medical Applications of Nuclear Physics
<section begin=32-Medical_Applications_of_Nuclear_Physics/> <section end=32-Medical_Applications_of_Nuclear_Physics/>
 * foo

33-Particle Physics
<section begin=33-Particle_Physics/> <section end=33-Particle_Physics/>
 * foo

34-Frontiers of Physics
<section begin=34-Frontiers_of_Physics/> <section end=34-Frontiers_of_Physics/>
 * foo