# Physics equations/Sheet/First semester

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/m$^3$, with pressure 10$^5$Pa. The density of water is 1000kg/m$^3$.
* Earth's mean radius ≈ 6371km, mass ≈ 6×10$^{24}$ kg, and gravitational acceleration = g ≈ 9.8m/s$^2$
* Universal gravitational constant = G ≈ 6.67×10$^{−11}$ m$^3$·kg$^{−1}$·s$^{−2}$
* Speed of sound ≈ 340m/s and the speed of light = c ≈ 3×10$^8$m/s
* One light-year ≈ 9.5×10$^{15}$m ≈ 63240AU (Astronomical unit)
* The electron has charge, e ≈ 1.6 × 10$^{−19}$C and mass ≈ 9.11 × 10$^{-31}$kg. 1eV = 1.602 × 10$^{-19}$J 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 = k$_B$≈ 1.38 × 10$^{-23}$ J K$^{−1}$ , and the gas constant is R = N$_A$k$_B$≈8.314 J  K$^{−1}$  mol$^{−1}$, where N$_A$≈ 6.02 × 10$^{23}$ is the Avogadro number.
* $k_{\mathrm {e} }={\frac {1}{4\pi \varepsilon _{0}}}\,$≈ 8.987× 10$^9$ 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=d$^2$x/dt$^2$.
The equations of motion for uniform acceleration are: $x=x_{0}+v_{0}t+{\tfrac {1}{2}}at^{2}$, and, $v=v_{0}+at$. Also, $v^{2}=v_{0}^{2}+2a\left(x-x_{0}\right)$, and, $x-x_{0}={\tfrac {1}{2}}(v_{0}+v)={\bar {v}}t$. Note that ${\bar {v}}={\tfrac {1}{2}}(v_{0}+v)$ only if the acceleration is uniform.
03-Two-Dimensional_Kinematics
| $x=x_{0}+v_{0x}\Delta t+{\frac {1}{2}}a_{x}\Delta t^{2}$ | $v_{x}=v_{0x}+a_{x}\Delta t$ | $v_{x}^{2}=v_{x0}^{2}+2a_{x}\Delta x$ |
| $y=y_{0}+v_{0y}\Delta t+{\frac {1}{2}}a_{y}\Delta t^{2}$ | $v_{y}=v_{0y}+a_{y}\Delta t$ | $v_{y}^{2}=v_{x0}^{2}+2a_{y}\Delta y$ |
$v^{2}=v_{0}^{2}+2a_{x}\Delta x+2a_{y}\Delta y$ ...in advanced notation this becomes $\Delta (v^{2})=2{\vec {a}}\cdot \Delta {\vec {\ell }}$.
In free fall we often set, a$_x$=0 and a$_y$= -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:
* The normal force, $N$, is a contact forces that is perpendicular to the surface,
* 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.
* 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, $g\approx 9.8m/s^{2}$.
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 μ$_k$ ("mew-sub-k") is the kinetic coefficient of friction, and N is the normal force.
* $f_{s}\leq \mu _{s}N$ approximates the maximum possible friction (called static friction) that can occur before the object begins to slide. Usually μ$_s$ > μ$_k$. Also, air drag often depends on speed, an effect this model fails to capture.
06-Uniform_Circular_Motion_and_Gravitation
* $a={\frac {v^{2}}{r}}=\omega v=\omega ^{2}r$ 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.
07-Work_and_Energy
* $KE={\frac {1}{2}}mv^{2}\,$ 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 θ.
* $\sum {\vec {F}}\cdot \Delta \ell$ 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
* ${\vec {p}}=m{\vec {v}}$ 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
The SI units for torque is the newton metre (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$_⊥$.
10-Rotational_Motion_and_Angular Momentum
| Linear motion | Angular motion |
| $x-x_{0}=v_{0}t+{\frac {1}{2}}at^{2}$ | $\theta -\theta _{0}=\omega _{0}t+{\frac {1}{2}}\alpha t^{2}$ |
| $v=v_{0}+at\,$ | $\omega =\omega _{0}+\alpha t\,$ |
| $x-x_{0}={\frac {1}{2}}(v_{0}+v)t$ | $\theta -\theta _{0}={\frac {1}{2}}(\omega _{0}+\omega )t$ |
| $v^{2}=v_{0}^{2}+2a(x-x_{0})\,$ | $\omega ^{2}=\omega _{0}^{2}+2\alpha (\theta -\theta _{0})$ |
The following table refers to rotation of a rigid body about a fixed axis: $\mathbf {s}$ is arclength, $\mathbf {r}$ is the distance from the axis to any point, and $\mathbf {a} _{\mathbf {t} }$ is the tangential acceleration, which is the component of the acceleration that is parallel to the motion. In contrast, the centripetal acceleration, $\mathbf {a} _{\mathbf {c} }=v^{2}/r=\omega ^{2}r$, is perpendicular to the motion. The component of the force parallel to the motion, or equivalently, perpendicular, to the line connecting the point of application to the axis is $\mathbf {F} _{\perp }$. The sum is over $\mathbf {j} \ =1\ \mathbf {to} \ N$ particles or points of application.
Analogy between Linear Motion and Rotational motion :
| Linear motion | Rotational motion | Defining equation |
| Displacement = $\mathbf {x}$ | Angular displacement = $\theta$ | $\theta =\mathbf {x} /\mathbf {r}$ |
| Velocity = $\mathbf {v}$ | Angular velocity = $\omega$ | $\omega =\mathbf {d} \theta /\mathbf {dt} =\mathbf {v} /\mathbf {r}$ |
| Acceleration = $\mathbf {a}$ | Angular acceleration = $\alpha$ | $\alpha =\mathbf {d} \omega /\mathbf {dt} =\mathbf {a_{\mathbf {t} }} /\mathbf {r}$ |
| Mass = $\mathbf {m}$ | Moment of Inertia = $\mathbf {I}$ | $\mathbf {I} =\sum \mathbf {m_{j}} \mathbf {r_{j}} ^{2}$ |
| Force = $\mathbf {F} =\mathbf {m} \mathbf {a}$ | Torque = $\tau =\mathbf {I} \alpha$ | $\tau =\sum \mathbf {r_{j}} \mathbf {F} _{\perp }\mathbf {_{j}} =\sum \mathbf {r_{\perp j}} \mathbf {F} _{\mathbf {_{j}} }$ |
| Momentum= $\mathbf {p} =\mathbf {m} \mathbf {v}$ | Angular momentum= $\mathbf {L} =\mathbf {I} \omega$ | $\mathbf {L} =\sum \mathbf {r_{j}} \mathbf {p} \mathbf {_{j}}$ |
| Kinetic energy = ${\frac {1}{2}}\mathbf {m} \mathbf {v} ^{2}$ | Kinetic energy = ${\frac {1}{2}}\mathbf {I} \omega ^{2}$ | ${\frac {1}{2}}\sum \mathbf {m_{j}} \mathbf {v_{j}} ^{2}={\frac {1}{2}}\sum \mathbf {m_{j}} \mathbf {r_{j}} ^{2}\omega ^{2}$ |
| Description | Moment(s) of inertia |
| Rod of length L and mass m (Axis of rotation at the end of the rod) | $I_{\mathrm {end} }={\frac {mL^{2}}{3}}\,\!$ |
| Solid cylinder of radius r, height h and mass m | $I_{z}={\frac {mr^{2}}{2}}\,\!$ $I_{x}=I_{y}={\frac {1}{12}}m\left(3r^{2}+h^{2}\right)$ |
| Sphere (hollow) of radius r and mass m | $I={\frac {2mr^{2}}{3}}\,\!$ |
| Ball (solid) of radius r and mass m | $I={\frac {2mr^{2}}{5}}\,\!$ |
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:
    $P=P_{0}+\rho gh$
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.
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, $v_{1}A_{1}=v_{2}A_{2}$ 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 $\Delta t$.
* $P_{1}+\rho gy_{1}+{\frac {1}{2}}\rho v_{1}^{2}=P_{2}+\rho gy_{2}+{\frac {1}{2}}\rho v_{2}^{2}$ 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
* $T_{C}=T_{K}-273.15$ converts from Celsius to Kelvins, and $T_{F}={\frac {9}{5}}T_{C}+32$ converts from Celsius to Fahrenheit.
* $PV=nRT=Nk_{B}T$ 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).
* N$_A$k$_B$=R where N$_A$= 6.02 × 10$^{23}$ is the Avogadro number. Boltzmann's constant can also be written in eV and Kelvins: k$_B$ ≈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.
* $v_{rms}={\sqrt {\frac {3k_{B}T}{m}}}={\sqrt {\overline {v^{2}}}}$ is the root-mean-square speed of atoms in an ideal gas.
* $E={\frac {\varpi }{2}}Nk_{B}T$ is the total energy of an ideal gas, where $\varpi =3\;$
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
* $Q=mc_{S}\Delta T$ is the heat required to change the temperature of a substance of mass, m. The change in temperature is ΔT. The specific heat, c$_S$, 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. L$_F$ is called the latent heat of fusion, and refers to the melting or freezing of the substance. L$_V$ is called the latent heat of vaporization, and refers to evaporation or condensation of a substance.
* ${\dot {Q}}={\frac {k_{c}A}{d}}\Delta T$ 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, k$_c$, 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, $0\leq \epsilon \leq 1$, 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
* 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.
* $S(V,T)={\frac {3Nk_{B}}{2}}\ln T+Nk_{B}\ln V+constant$, 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.
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.
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 ΔQ 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,
       $\int _{Vi}^{Vf}PdV=\int _{Vi}^{Vf}nRT{\frac {dV}{V}}=nRT\int _{Vi}^{Vf}{\frac {dV}{V}}=nRT\ln {\frac {V_{f}}{V_{i}}}$
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, k$_s$.
* $\omega _{0}={\sqrt {\frac {g}{L}}}={\frac {2\pi }{T}}$ 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:
* $v(t)=dx/dt=-\omega _{0}x_{0}\sin \left(\omega _{0}t-\varphi \right)=v_{0}\cos \left(\omega _{0}t+...\right)$, where $v_{0}=\omega _{0}x_{0}$ is maximum velocity.
* $a(t)=dv/dt=-\omega _{0}v_{0}\cos \left(\omega _{0}t-\varphi \right)=a_{0}\cos \left(\omega _{0}t+...\right)$, where $a_{0}=\omega _{0}v_{0}=\omega _{0}^{2}x_{0}$, is maximum acceleration.
* $F_{0}=ma_{0}$, 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), ${\frac {d^{2}x}{dt^{2}}}=-\omega _{0}^{2}x(t)$
* $f\lambda =v_{p}$ relates the frequency, f, wavelength, λ,and the the phase speed, v$_p$ of the wave (also written as v$_w$) 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
* $v_{s}={\sqrt {\frac {T}{273}}}\cdot 331{\text{m/s}}$ 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, γ = 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).
* ↑ https://en.wikipedia.org/w/index.php?title=Torque&oldid=582917749
* ↑ "Linear Motion vs Rotational motion" (PDF).
* ↑ https://en.wikipedia.org/w/index.php?title=List_of_moments_of_inertia&oldid=582953751