All Class 11 Physics formulas

The formulas from 14 chapters, in one place to revise from or print. Open a chapter's own sheet to see where students usually slip up.

1. Units and Measurement

Errors

Absolute error
Δai=∣amean−ai∣\displaystyle \Delta a_i = |a_{\text{mean}} - a_i|
Relative error
δa=Δameanamean\displaystyle \delta a = \frac{\Delta a_{\text{mean}}}{a_{\text{mean}}}

Multiply by 100 for percentage error.

Error in a sum or difference
ΔZ=ΔA+ΔB\displaystyle \Delta Z = \Delta A + \Delta B

Absolute errors always add.

Error in a product or quotient
ΔZZ=ΔAA+ΔBB\displaystyle \frac{\Delta Z}{Z} = \frac{\Delta A}{A} + \frac{\Delta B}{B}

Relative errors add.

Error in a power
Z=ApBqCr  ⇒  ΔZZ=pΔAA+qΔBB+rΔCC\displaystyle Z = \frac{A^p B^q}{C^r} \;\Rightarrow\; \frac{\Delta Z}{Z} = p\frac{\Delta A}{A} + q\frac{\Delta B}{B} + r\frac{\Delta C}{C}

Dimensions

Force
[F]=[MLT−2]\displaystyle [F] = [\mathrm{M L T^{-2}}]
Energy
[E]=[ML2T−2]\displaystyle [E] = [\mathrm{M L^2 T^{-2}}]
Power
[P]=[ML2T−3]\displaystyle [P] = [\mathrm{M L^2 T^{-3}}]
Pressure
[p]=[ML−1T−2]\displaystyle [p] = [\mathrm{M L^{-1} T^{-2}}]

2. Motion in a Straight Line

Definitions

Average velocity
vˉ=ΔxΔt\displaystyle \bar v = \frac{\Delta x}{\Delta t}
Instantaneous velocity
v=dxdt\displaystyle v = \frac{dx}{dt}
Instantaneous acceleration
a=dvdt=vdvdx\displaystyle a = \frac{dv}{dt} = v\frac{dv}{dx}

Equations of motion (constant acceleration)

First equation
v=u+at\displaystyle v = u + at
Second equation
s=ut+12at2\displaystyle s = ut + \tfrac12 at^2
Third equation
v2=u2+2as\displaystyle v^2 = u^2 + 2as
Distance in the nth second
sn=u+a2(2n−1)\displaystyle s_n = u + \frac{a}{2}(2n - 1)

Free fall and graphs

Falling from rest
v=gt,h=12gt2,v2=2gh\displaystyle v = gt, \quad h = \tfrac12 gt^2, \quad v^2 = 2gh
Relative velocity
vBA=vB−vA\displaystyle v_{BA} = v_B - v_A
Reading graphs
v=slope of x-t,a=slope of v-t,Δx=area under v-t\displaystyle v = \text{slope of } x\text{-}t, \quad a = \text{slope of } v\text{-}t, \quad \Delta x = \text{area under } v\text{-}t

3. Motion in a Plane

Vectors

Resultant of two vectors
R=A2+B2+2ABcos⁡θ\displaystyle R = \sqrt{A^2 + B^2 + 2AB\cos\theta}
Direction of the resultant
tan⁡α=Bsin⁡θA+Bcos⁡θ\displaystyle \tan\alpha = \frac{B\sin\theta}{A + B\cos\theta}

α is the angle from A.

Components
Ax=Acos⁡θ,Ay=Asin⁡θ\displaystyle A_x = A\cos\theta, \quad A_y = A\sin\theta

Projectile motion

Time of flight
T=2usin⁡θg\displaystyle T = \frac{2u\sin\theta}{g}
Maximum height
H=u2sin⁡2θ2g\displaystyle H = \frac{u^2\sin^2\theta}{2g}
Horizontal range
R=u2sin⁡2θg\displaystyle R = \frac{u^2\sin 2\theta}{g}

Largest at θ = 45°. Angles θ and 90° − θ give the same range.

Path equation
y=xtan⁡θ−gx22u2cos⁡2θ\displaystyle y = x\tan\theta - \frac{g x^2}{2u^2\cos^2\theta}

Circular motion

Angular speed
ω=ΔθΔt=2πT=2πν\displaystyle \omega = \frac{\Delta\theta}{\Delta t} = \frac{2\pi}{T} = 2\pi\nu
Linear and angular speed
v=rω\displaystyle v = r\omega
Centripetal acceleration
ac=v2r=rω2\displaystyle a_c = \frac{v^2}{r} = r\omega^2

4. Laws of Motion

Newton's laws and momentum

Second law
F⃗=dp⃗dt=ma⃗\displaystyle \vec F = \frac{d\vec p}{dt} = m\vec a

The form with a holds when mass is constant.

Momentum
p⃗=mv⃗\displaystyle \vec p = m\vec v
Impulse
J⃗=F⃗ Δt=Δp⃗\displaystyle \vec J = \vec F\,\Delta t = \Delta\vec p
Conservation of momentum
m1u⃗1+m2u⃗2=m1v⃗1+m2v⃗2\displaystyle m_1\vec u_1 + m_2\vec u_2 = m_1\vec v_1 + m_2\vec v_2

Holds when net external force is zero.

Friction

Limiting static friction
fs,max⁡=μsN\displaystyle f_{s,\max} = \mu_s N
Kinetic friction
fk=μkN\displaystyle f_k = \mu_k N
Block on a rough incline
a=g(sin⁡θ−μkcos⁡θ)\displaystyle a = g(\sin\theta - \mu_k\cos\theta)

Sliding down. It only slides if tan θ exceeds μₛ.

Circular motion

Centripetal force
Fc=mv2r\displaystyle F_c = \frac{mv^2}{r}
Maximum speed on a level road
vmax⁡=μsrg\displaystyle v_{\max} = \sqrt{\mu_s r g}
Ideal speed on a banked road
v0=rgtan⁡θ\displaystyle v_0 = \sqrt{r g \tan\theta}

No friction needed at this speed.

Maximum speed on a banked road
vmax⁡=rg μs+tan⁡θ1−μstan⁡θ\displaystyle v_{\max} = \sqrt{r g\,\frac{\mu_s + \tan\theta}{1 - \mu_s\tan\theta}}

5. Work, Energy and Power

Work and energy

Work by a constant force
W=F⃗⋅d⃗=Fdcos⁡θ\displaystyle W = \vec F\cdot\vec d = Fd\cos\theta
Work by a variable force
W=∫xixfF dx\displaystyle W = \int_{x_i}^{x_f} F\,dx
Kinetic energy
K=12mv2=p22m\displaystyle K = \tfrac12 mv^2 = \frac{p^2}{2m}
Work-energy theorem
Wnet=ΔK\displaystyle W_{\text{net}} = \Delta K
Gravitational potential energy
U=mgh\displaystyle U = mgh

Near Earth's surface.

Spring potential energy
U=12kx2\displaystyle U = \tfrac12 kx^2
Spring force
F=−kx\displaystyle F = -kx

Power

Average power
Pav=Wt\displaystyle P_{\text{av}} = \frac{W}{t}
Instantaneous power
P=F⃗⋅v⃗\displaystyle P = \vec F\cdot\vec v

Collisions

Coefficient of restitution
e=v2−v1u1−u2\displaystyle e = \frac{v_2 - v_1}{u_1 - u_2}

e = 1 is elastic, and e = 0 is perfectly inelastic.

1D elastic collision
v1=(m1−m2)u1+2m2u2m1+m2\displaystyle v_1 = \frac{(m_1 - m_2)u_1 + 2m_2u_2}{m_1 + m_2}

Swap the subscripts to get v₂.

Perfectly inelastic collision
v=m1u1+m2u2m1+m2\displaystyle v = \frac{m_1u_1 + m_2u_2}{m_1 + m_2}

6. System of Particles and Rotational Motion

Centre of mass

Discrete particles
r⃗cm=∑mir⃗i∑mi\displaystyle \vec r_{\text{cm}} = \frac{\sum m_i\vec r_i}{\sum m_i}
Continuous body
r⃗cm=1M∫r⃗ dm\displaystyle \vec r_{\text{cm}} = \frac{1}{M}\int \vec r\,dm

Rotation

Torque
τ⃗=r⃗×F⃗,τ=rFsin⁡θ\displaystyle \vec\tau = \vec r\times\vec F, \quad \tau = rF\sin\theta
Angular momentum
L⃗=r⃗×p⃗,L=Iω\displaystyle \vec L = \vec r\times\vec p, \quad L = I\omega
Rotational second law
τ=Iα=dLdt\displaystyle \tau = I\alpha = \frac{dL}{dt}
Rotational kinetic energy
K=12Iω2\displaystyle K = \tfrac12 I\omega^2
Rotational power
P=τω\displaystyle P = \tau\omega
Equations of rotation
ω=ω0+αt,θ=ω0t+12αt2,ω2=ω02+2αθ\displaystyle \omega = \omega_0 + \alpha t, \quad \theta = \omega_0 t + \tfrac12\alpha t^2, \quad \omega^2 = \omega_0^2 + 2\alpha\theta

Moment of inertia

Definition
I=∑miri2\displaystyle I = \sum m_i r_i^2
Parallel axis theorem
I=Icm+Md2\displaystyle I = I_{\text{cm}} + Md^2
Perpendicular axis theorem
Iz=Ix+Iy\displaystyle I_z = I_x + I_y

For flat bodies only.

Ring, about its central axis
I=MR2\displaystyle I = MR^2
Disc, about its central axis
I=12MR2\displaystyle I = \tfrac12 MR^2
Solid sphere, about a diameter
I=25MR2\displaystyle I = \tfrac25 MR^2
Hollow sphere, about a diameter
I=23MR2\displaystyle I = \tfrac23 MR^2
Rod, about its centre
I=112ML2\displaystyle I = \tfrac{1}{12}ML^2
Rod, about one end
I=13ML2\displaystyle I = \tfrac13 ML^2

Rolling without slipping

Condition
vcm=Rω\displaystyle v_{\text{cm}} = R\omega
Total kinetic energy
K=12mv2(1+k2R2)\displaystyle K = \tfrac12 mv^2\left(1 + \frac{k^2}{R^2}\right)

k is the radius of gyration, from I = mk².

Acceleration down an incline
a=gsin⁡θ1+k2/R2\displaystyle a = \frac{g\sin\theta}{1 + k^2/R^2}

7. Gravitation

Force and acceleration

Newton's law of gravitation
F=Gm1m2r2\displaystyle F = \frac{Gm_1m_2}{r^2}
Acceleration due to gravity
g=GMR2\displaystyle g = \frac{GM}{R^2}
At height h
gh=g(1+h/R)2≈g(1−2hR)\displaystyle g_h = \frac{g}{(1 + h/R)^2} \approx g\left(1 - \frac{2h}{R}\right)

The approximation needs h much smaller than R.

At depth d
gd=g(1−dR)\displaystyle g_d = g\left(1 - \frac{d}{R}\right)

Energy and escape

Gravitational potential energy
U=−GMmr\displaystyle U = -\frac{GMm}{r}
Gravitational potential
V=−GMr\displaystyle V = -\frac{GM}{r}
Escape speed
ve=2GMR=2gR\displaystyle v_e = \sqrt{\frac{2GM}{R}} = \sqrt{2gR}

Orbits

Orbital speed
vo=GMr\displaystyle v_o = \sqrt{\frac{GM}{r}}

Close to the surface, vₑ = √2 × vₒ.

Time period
T=2πr3GM\displaystyle T = 2\pi\sqrt{\frac{r^3}{GM}}
Kepler's third law
T2∝r3\displaystyle T^2 \propto r^3
Energy of a satellite
E=−GMm2r,K=GMm2r,U=−GMmr\displaystyle E = -\frac{GMm}{2r}, \quad K = \frac{GMm}{2r}, \quad U = -\frac{GMm}{r}

8. Mechanical Properties of Solids

Stress and strain

Stress
σ=FA\displaystyle \sigma = \frac{F}{A}
Longitudinal strain
ε=ΔLL\displaystyle \varepsilon = \frac{\Delta L}{L}
Hooke's law
stress=modulus×strain\displaystyle \text{stress} = \text{modulus} \times \text{strain}

Within the elastic limit.

Moduli of elasticity

Young's modulus
Y=FLA ΔL\displaystyle Y = \frac{FL}{A\,\Delta L}
Shear modulus
G=F/AΔx/L=F/Aθ\displaystyle G = \frac{F/A}{\Delta x / L} = \frac{F/A}{\theta}
Bulk modulus
B=−pΔV/V\displaystyle B = -\frac{p}{\Delta V / V}
Compressibility
k=1B\displaystyle k = \frac{1}{B}
Elastic energy per unit volume
u=12×stress×strain\displaystyle u = \tfrac12 \times \text{stress} \times \text{strain}

9. Mechanical Properties of Fluids

Pressure and buoyancy

Pressure at depth
p=p0+ρgh\displaystyle p = p_0 + \rho g h
Pascal's law (hydraulic lift)
F1A1=F2A2\displaystyle \frac{F_1}{A_1} = \frac{F_2}{A_2}
Archimedes' principle
Fb=ρfluid Vdisplaced g\displaystyle F_b = \rho_{\text{fluid}}\, V_{\text{displaced}}\, g

Flowing fluids

Continuity equation
A1v1=A2v2\displaystyle A_1v_1 = A_2v_2
Bernoulli's equation
p+12ρv2+ρgh=constant\displaystyle p + \tfrac12\rho v^2 + \rho g h = \text{constant}

For steady, incompressible, non-viscous flow.

Torricelli's law
v=2gh\displaystyle v = \sqrt{2gh}

Viscosity

Viscous force
F=ηAdvdx\displaystyle F = \eta A\frac{dv}{dx}
Stokes' law
F=6πηrv\displaystyle F = 6\pi\eta r v
Terminal velocity
vt=2r2(ρ−σ)g9η\displaystyle v_t = \frac{2r^2(\rho - \sigma)g}{9\eta}

ρ is the sphere's density and σ the fluid's.

Reynolds number
Re=ρvdη\displaystyle R_e = \frac{\rho v d}{\eta}

Surface tension

Surface tension
S=FL\displaystyle S = \frac{F}{L}
Excess pressure in a drop
Δp=2Sr\displaystyle \Delta p = \frac{2S}{r}
Excess pressure in a soap bubble
Δp=4Sr\displaystyle \Delta p = \frac{4S}{r}

A bubble has two surfaces.

Capillary rise
h=2Scos⁡θρgr\displaystyle h = \frac{2S\cos\theta}{\rho g r}

10. Thermal Properties of Matter

Temperature and expansion

Temperature scales
TC100=TF−32180,TK=TC+273.15\displaystyle \frac{T_C}{100} = \frac{T_F - 32}{180}, \quad T_K = T_C + 273.15
Linear expansion
ΔL=αL ΔT\displaystyle \Delta L = \alpha L\,\Delta T
Area and volume expansion
ΔA=βA ΔT,ΔV=γV ΔT\displaystyle \Delta A = \beta A\,\Delta T, \quad \Delta V = \gamma V\,\Delta T
Relation between coefficients
β=2α,γ=3α\displaystyle \beta = 2\alpha, \quad \gamma = 3\alpha

For isotropic solids.

Calorimetry

Heat and specific heat
Q=mc ΔT\displaystyle Q = mc\,\Delta T
Latent heat
Q=mL\displaystyle Q = mL

Heat transfer

Conduction
Qt=kA(T1−T2)L\displaystyle \frac{Q}{t} = \frac{kA(T_1 - T_2)}{L}
Stefan-Boltzmann law
P=eσAT4\displaystyle P = e\sigma A T^4
Wien's displacement law
λmT=b\displaystyle \lambda_m T = b
Newton's law of cooling
dTdt=−k(T−Ts)\displaystyle \frac{dT}{dt} = -k(T - T_s)

11. Thermodynamics

First law

First law of thermodynamics
ΔQ=ΔU+ΔW\displaystyle \Delta Q = \Delta U + \Delta W

Here W is the work done by the gas.

Work by a gas
W=∫V1V2p dV\displaystyle W = \int_{V_1}^{V_2} p\,dV
Change in internal energy
ΔU=nCV ΔT\displaystyle \Delta U = nC_V\,\Delta T

For an ideal gas, in any process.

Mayer's relation
Cp−CV=R\displaystyle C_p - C_V = R
Ratio of specific heats
γ=CpCV\displaystyle \gamma = \frac{C_p}{C_V}

Processes (ideal gas)

Isothermal work
W=nRTln⁡V2V1\displaystyle W = nRT\ln\frac{V_2}{V_1}
Adiabatic relation
pVγ=constant\displaystyle pV^\gamma = \text{constant}
Adiabatic work
W=nR(T1−T2)γ−1\displaystyle W = \frac{nR(T_1 - T_2)}{\gamma - 1}
Isobaric work
W=p ΔV\displaystyle W = p\,\Delta V
Isochoric work
W=0\displaystyle W = 0

Engines

Efficiency of a heat engine
η=WQ1=1−Q2Q1\displaystyle \eta = \frac{W}{Q_1} = 1 - \frac{Q_2}{Q_1}
Carnot efficiency
η=1−T2T1\displaystyle \eta = 1 - \frac{T_2}{T_1}

Temperatures in kelvin.

Coefficient of performance
β=Q2W\displaystyle \beta = \frac{Q_2}{W}

For a refrigerator.

12. Kinetic Theory

Ideal gas

Ideal gas law
pV=nRT=NkBT\displaystyle pV = nRT = Nk_BT
Pressure from kinetic theory
p=13ρ v2‾\displaystyle p = \tfrac13\rho\,\overline{v^2}
Average kinetic energy of a molecule
Kˉ=32kBT\displaystyle \bar K = \tfrac32 k_BT

Molecular speeds

RMS speed
vrms=3RTM\displaystyle v_{\text{rms}} = \sqrt{\frac{3RT}{M}}

M is the molar mass in kg/mol.

Mean speed
vmean=8RTπM\displaystyle v_{\text{mean}} = \sqrt{\frac{8RT}{\pi M}}
Most probable speed
vmp=2RTM\displaystyle v_{\text{mp}} = \sqrt{\frac{2RT}{M}}

Degrees of freedom

Energy per degree of freedom
E=12kBT\displaystyle E = \tfrac12 k_BT
Specific heats from f
CV=f2R,Cp=(f2+1)R,γ=1+2f\displaystyle C_V = \frac{f}{2}R, \quad C_p = \left(\frac{f}{2} + 1\right)R, \quad \gamma = 1 + \frac{2}{f}

f = 3 for monatomic and 5 for a rigid diatomic gas.

Mean free path
λ=12 nπd2\displaystyle \lambda = \frac{1}{\sqrt2\,n\pi d^2}

13. Oscillations

Motion

Displacement
x=Asin⁡(ωt+ϕ)\displaystyle x = A\sin(\omega t + \phi)
Velocity
v=ωA2−x2\displaystyle v = \omega\sqrt{A^2 - x^2}

Largest at the mean position, where v = Aω.

Acceleration
a=−ω2x\displaystyle a = -\omega^2 x

Largest at the extremes, where |a| = Aω².

Angular frequency
ω=2πν=2πT\displaystyle \omega = 2\pi\nu = \frac{2\pi}{T}

Energy

Kinetic energy
K=12mω2(A2−x2)\displaystyle K = \tfrac12 m\omega^2(A^2 - x^2)
Potential energy
U=12mω2x2\displaystyle U = \tfrac12 m\omega^2 x^2
Total energy
E=12mω2A2\displaystyle E = \tfrac12 m\omega^2 A^2

Stays constant.

Common systems

Spring and mass
T=2πmk\displaystyle T = 2\pi\sqrt{\frac{m}{k}}
Simple pendulum
T=2πLg\displaystyle T = 2\pi\sqrt{\frac{L}{g}}

For small angles.

Springs in series
1k=1k1+1k2\displaystyle \frac{1}{k} = \frac{1}{k_1} + \frac{1}{k_2}
Springs in parallel
k=k1+k2\displaystyle k = k_1 + k_2

14. Waves

Waves

Wave equation
y=asin⁡(kx−ωt+ϕ)\displaystyle y = a\sin(kx - \omega t + \phi)
Wave number and speed
k=2πλ,v=νλ=ωk\displaystyle k = \frac{2\pi}{\lambda}, \quad v = \nu\lambda = \frac{\omega}{k}
Speed on a string
v=Tμ\displaystyle v = \sqrt{\frac{T}{\mu}}

μ is mass per unit length.

Speed of sound (Laplace)
v=γPρ\displaystyle v = \sqrt{\frac{\gamma P}{\rho}}

Standing waves

String fixed at both ends
νn=nv2L,n=1,2,3,…\displaystyle \nu_n = \frac{nv}{2L}, \quad n = 1, 2, 3, \dots
Open pipe
νn=nv2L,n=1,2,3,…\displaystyle \nu_n = \frac{nv}{2L}, \quad n = 1, 2, 3, \dots
Closed pipe
νn=(2n−1)v4L,n=1,2,3,…\displaystyle \nu_n = \frac{(2n - 1)v}{4L}, \quad n = 1, 2, 3, \dots

Only odd harmonics exist.

Beats

Beat frequency
νbeat=∣ν1−ν2∣\displaystyle \nu_{\text{beat}} = |\nu_1 - \nu_2|

Try it on your weakest chapter.

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