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CalibratePhysics

Chapter 1

Rotational Dynamics

Maharashtra HSC · 11 subtopics · textbook pages 1–25

Formula SheetEvery formula this chapter can be examined on, in one table.

Kinematics of Circular Motion

FormulaSymbols, units and conditions
ω=dθdt,α=dωdt\omega = \dfrac{d\theta}{dt}, \qquad \alpha = \dfrac{d\omega}{dt}
  • θ\theta is angular displacement (rad), ω\omega angular velocity (rad/s), α\alpha angular acceleration (rad/s2^2). Direction of ω⃗\vec\omega and α⃗\vec\alpha is along the axis of rotation, by the right-hand thumb rule.
v⃗=ω⃗×r⃗,v=ωr\vec v = \vec\omega \times \vec r, \qquad v = \omega r
  • r⃗\vec r is the radius vector from the centre of the circle; vv is the tangential (linear) speed in m/s.
ω=2πT=2πn\omega = \dfrac{2\pi}{T} = 2\pi n
  • TT = periodic time (s), nn = frequency (rev/s, i.e. Hz). Conversions used in every numerical: 1 rev =2π= 2\pi rad, 1 rpm =160= \dfrac{1}{60} rps, 1∘=π1801^\circ = \dfrac{\pi}{180} rad.
ω=ω0+αt,θ=ω0t+12αt2,ω2=ω02+2αθ\omega = \omega_0 + \alpha t, \qquad \theta = \omega_0 t + \dfrac{1}{2}\alpha t^2, \qquad \omega^2 = \omega_0^2 + 2\alpha\theta
  • Valid only when α\alpha is constant and along the axis. For NN revolutions, θ=2πN\theta = 2\pi N rad.
ar=ω2r=v2r=vω,a⃗r=−ω2r⃗a_r = \omega^2 r = \dfrac{v^2}{r} = v\omega, \qquad \vec a_r = -\omega^2\vec r
  • Radial (centripetal) acceleration, m/s2^2, always directed towards the centre.
aT=dvdt=rα,a=ar2+aT2a_T = \dfrac{dv}{dt} = r\alpha, \qquad a = \sqrt{a_r^2 + a_T^2}
  • Tangential acceleration changes only the speed. For U.C.M., aT=0a_T = 0 and a=ara = a_r.

Dynamics of Circular Motion

FormulaSymbols, units and conditions
F⃗CP=−mω2r⃗,FCP=mrω2=mv2r=mvω\vec F_{CP} = -m\omega^2\vec r, \qquad F_{CP} = mr\omega^2 = \dfrac{mv^2}{r} = mv\omega
  • Centripetal force: the resultant of all the real forces, directed towards the centre. SI unit newton (N).
F⃗CF=+mω2r⃗,FCF=mv2r\vec F_{CF} = +m\omega^2\vec r, \qquad F_{CF} = \dfrac{mv^2}{r}
  • Centrifugal force: pseudo force of the same magnitude, away from the centre, used only in the non-inertial frame attached to the rotating body.

Applications of Uniform Circular Motion

FormulaSymbols, units and conditions
N=mg,fs=mv2r,fsN=v2rgN = mg, \qquad f_s = \dfrac{mv^2}{r}, \qquad \dfrac{f_s}{N} = \dfrac{v^2}{rg}
  • Vehicle on a horizontal (unbanked) circular track of radius rr; static friction supplies the centripetal force.
vmax=μsrg,μs, min=v2rgv_{max} = \sqrt{\mu_s r g}, \qquad \mu_{s,\,min} = \dfrac{v^2}{rg}
  • Upper speed limit on an unbanked track; μs\mu_s = coefficient of static friction. Independent of the mass.
N=mv2r,fs=mg,vmin=rgμs,Tmax=2πrvminN = \dfrac{mv^2}{r}, \qquad f_s = mg, \qquad v_{min} = \sqrt{\dfrac{rg}{\mu_s}}, \qquad T_{max} = \dfrac{2\pi r}{v_{min}}
  • Well (wall) of death, a vertical cylindrical wall of radius rr. Here NN is horizontal and centripetal, friction is vertically up. TmaxT_{max} is the largest period (slowest allowed rotation); nmin=vmin2πrn_{min} = \dfrac{v_{min}}{2\pi r}.
Ncos⁡θ=mg,Nsin⁡θ=mv2r,tan⁡θ=v2rgN\cos\theta = mg, \qquad N\sin\theta = \dfrac{mv^2}{r}, \qquad \tan\theta = \dfrac{v^2}{rg}
  • Frictionless banked road of radius rr and banking angle θ\theta.
vs=rgtan⁡θ,θ=tan⁡−1 ⁣(v2rg)v_s = \sqrt{rg\tan\theta}, \qquad \theta = \tan^{-1}\!\left(\dfrac{v^2}{rg}\right)
  • vsv_s is the most safe speed (neither a maximum nor a minimum); it is independent of the mass of the vehicle.
h=lsin⁡θh = l\sin\theta
  • Elevation of the outer edge (or outer rail) above the inner one; ll = width of the road or the rail gauge in metres. Length of a circular track =2πr= 2\pi r.
vmin=rg(tan⁡θ−μs1+μstan⁡θ),vmax=rg(tan⁡θ+μs1−μstan⁡θ)v_{min} = \sqrt{rg\left(\dfrac{\tan\theta-\mu_s}{1+\mu_s\tan\theta}\right)}, \qquad v_{max} = \sqrt{rg\left(\dfrac{\tan\theta+\mu_s}{1-\mu_s\tan\theta}\right)}
  • Speed limits on a rough banked road. If μs≥tan⁡θ\mu_s \ge \tan\theta then vmin=0v_{min}=0; if μs=cot⁡θ\mu_s = \cot\theta (i.e. θ≥45∘\theta \ge 45^\circ since (μs)max=1(\mu_s)_{max}=1) there is no upper limit.
T0cos⁡θ=mg,T0sin⁡θ=mv2r=mrω2,tan⁡θ=v2rgT_0\cos\theta = mg, \qquad T_0\sin\theta = \dfrac{mv^2}{r} = mr\omega^2, \qquad \tan\theta = \dfrac{v^2}{rg}
  • Conical pendulum: bob of mass mm, string of length LL, semi-vertical angle θ\theta, force due to tension T0T_0.
r=Lsin⁡θ,cos⁡θ=hL=hr2+h2,T0=mgcos⁡θr = L\sin\theta, \qquad \cos\theta = \dfrac{h}{L} = \dfrac{h}{\sqrt{r^2+h^2}}, \qquad T_0 = \dfrac{mg}{\cos\theta}
  • hh = vertical depth of the bob below the support.
ω=gLcos⁡θ,Period T=2πLcos⁡θg,n=12πgLcos⁡θ\omega = \sqrt{\dfrac{g}{L\cos\theta}}, \qquad \text{Period } T = 2\pi\sqrt{\dfrac{L\cos\theta}{g}}, \qquad n = \dfrac{1}{2\pi}\sqrt{\dfrac{g}{L\cos\theta}}
  • Period and frequency of a conical pendulum. Both are independent of the mass of the bob.
tan⁡θ=v2rg\tan\theta = \dfrac{v^2}{rg}
  • Angle with the vertical at which a two-wheeler rider must lean on an unbanked circular road of radius rr.

Vertical Circular Motion (governed by gravity)

FormulaSymbols, units and conditions
mg+TA=mvA2r,(vA)min=rg(TA=0)mg + T_A = \dfrac{mv_A^2}{r}, \qquad (v_A)_{min} = \sqrt{rg} \quad (T_A = 0)
  • Uppermost point A of a vertical circle of radius rr (string or sphere of death — replace TT by NN).
TB−mg=mvB2r,(vB)min=5rgT_B - mg = \dfrac{mv_B^2}{r}, \qquad (v_B)_{min} = \sqrt{5rg}
  • Lowermost point B.
TC=mvC2r,(vC)min=(vD)min=3rgT_C = \dfrac{mv_C^2}{r}, \qquad (v_C)_{min} = (v_D)_{min} = \sqrt{3rg}
  • Midway (string horizontal) positions C and D.
vB2−vA2=4rg,vB2−vC2=2rgv_B^2 - v_A^2 = 4rg, \qquad v_B^2 - v_C^2 = 2rg
  • From energy conservation over vertical drops 2r2r and rr respectively.
TB−TA=6mg,TC−TA=TD−TA=3mgT_B - T_A = 6mg, \qquad T_C - T_A = T_D - T_A = 3mg
  • Difference of extreme tensions depends only on the weight — independent of vv and rr.
T=mv2r+mgcos⁡θT = \dfrac{mv^2}{r} + mg\cos\theta
  • Force due to tension at an arbitrary position, θ\theta measured from the lowest point. Vertical rise from the lowest point is r(1−cos⁡θ)r(1-\cos\theta).
(vlowermost)min=4rg=2rg,(vmidway)min=2rg,(vuppermost)min=0(v_{lowermost})_{min} = \sqrt{4rg} = 2\sqrt{rg}, \qquad (v_{midway})_{min} = \sqrt{2rg}, \qquad (v_{uppermost})_{min} = 0
  • Bob tied to a rigid rod instead of a string. Here too Tlowermost−Tuppermost=6mgT_{lowermost} - T_{uppermost} = 6mg.
mg−N=mv2r,vmax=rgmg - N = \dfrac{mv^2}{r}, \qquad v_{max} = \sqrt{rg}
  • Vehicle at the top of a convex over-bridge of radius of curvature rr; contact is just lost when N=0N = 0.

Moment of Inertia

FormulaSymbols, units and conditions
I=∑i=1Nmiri2=∫r2 dmI = \sum_{i=1}^{N} m_i r_i^2 = \int r^2\,dm
  • mim_i = mass of the iith particle, rir_i = its perpendicular distance from the axis. SI unit kg m2^2; dimensions [M1L2T0][M^1L^2T^0].
Rotational K.E.=12Iω2\text{Rotational K.E.} = \dfrac{1}{2}I\omega^2
  • Analogous to 12mv2\dfrac{1}{2}mv^2.
ΔE=12I(ω22−ω12)=2π2I(n22−n12)\Delta E = \dfrac{1}{2}I\left(\omega_2^2-\omega_1^2\right) = 2\pi^2 I\left(n_2^2-n_1^2\right)
  • Work done in changing the angular speed of a body of moment of inertia II.
  • ObjectAxisMoment of inertia
  • Thin ring, hollow cylinderCentralMR2MR^2
  • Thin ringDiameter12MR2\dfrac{1}{2}MR^2
  • Annular ring, thick hollow cylinderCentral12M(r12+r22)\dfrac{1}{2}M(r_1^2+r_2^2)
  • Uniform disc, solid cylinderCentral12MR2\dfrac{1}{2}MR^2
  • Uniform discDiameter14MR2\dfrac{1}{4}MR^2
  • Thin walled hollow sphereCentral23MR2\dfrac{2}{3}MR^2
  • Solid sphereCentral25MR2\dfrac{2}{5}MR^2
  • Uniform spherical shellCentral25Mr25−r15r23−r13\dfrac{2}{5}M\dfrac{r_2^5-r_1^5}{r_2^3-r_1^3}
  • Thin uniform rod, rectangular plateTransverse, through centre112ML2\dfrac{1}{12}ML^2
  • Thin uniform rod, rectangular plateTransverse, about one end13ML2\dfrac{1}{3}ML^2
  • Uniform plate or parallelepipedCentral112M(L2+b2)\dfrac{1}{12}M(L^2+b^2)
  • Uniform solid right circular coneCentral310MR2\dfrac{3}{10}MR^2
  • Uniform hollow right circular coneCentral12MR2\dfrac{1}{2}MR^2
I=M(R24+L212)I = M\left(\dfrac{R^2}{4}+\dfrac{L^2}{12}\right)
  • Solid cylinder of radius RR and length LL, about a transverse axis through its centre (perpendicular to its length).
M=ρV=43πR3ρ(sphere),M=σπR2(disc)M = \rho V = \dfrac{4}{3}\pi R^3\rho \quad \text{(sphere)}, \qquad M = \sigma \pi R^2 \quad \text{(disc)}
  • ρ\rho = volume density (kg/m3^3), σ\sigma = surface density (kg/m2^2). Hence, for a solid sphere, Itangent=2815πR5ρI_{tangent} = \dfrac{28}{15}\pi R^5\rho, and for a disc, IC=12πR4σI_C = \dfrac{1}{2}\pi R^4\sigma.

Radius of Gyration

FormulaSymbols, units and conditions
I=MK2,K=IMI = MK^2, \qquad K = \sqrt{\dfrac{I}{M}}
  • KK = radius of gyration (m): the distance from the axis at which the whole mass may be supposed concentrated to give the same II.
Kring=R,Kdisc=R2,Krod, end=L3,Ksolid sphere=R25K_{ring} = R, \qquad K_{disc} = \dfrac{R}{\sqrt2}, \qquad K_{rod,\,end} = \dfrac{L}{\sqrt3}, \qquad K_{solid\ sphere} = R\sqrt{\dfrac{2}{5}}—

Theorem of Parallel Axes and Theorem of Perpendicular Axes

FormulaSymbols, units and conditions
IO=IC+Mh2,KO2=KC2+h2I_O = I_C + Mh^2, \qquad K_O^2 = K_C^2 + h^2
  • Parallel axes: ICI_C about an axis through the centre of mass, hh = distance between the two parallel axes. Applies to any object.
Iz=Ix+IyI_z = I_x + I_y
  • Perpendicular axes: applies to a laminar (two-dimensional) object only; xx, yy lie in its plane, zz is perpendicular to it, and all three are concurrent.
Idisc, tangent in plane=54MR2,Idisc, tangent perp.=32MR2I_{disc,\,tangent\ in\ plane} = \dfrac{5}{4}MR^2, \qquad I_{disc,\,tangent\ perp.} = \dfrac{3}{2}MR^2—
Iring, tangent in plane=32MR2,Isphere, tangent=75MR2I_{ring,\,tangent\ in\ plane} = \dfrac{3}{2}MR^2, \qquad I_{sphere,\,tangent} = \dfrac{7}{5}MR^2—

Angular Momentum

FormulaSymbols, units and conditions
L⃗=r⃗×p⃗,L=prsin⁡θ=mvrsin⁡θ\vec L = \vec r\times\vec p, \qquad L = pr\sin\theta = mvr\sin\theta
  • θ\theta = smaller angle between r⃗\vec r and p⃗\vec p. SI unit kg m2^2/s; dimensions [M1L2T−1][M^1L^2T^{-1}].
L=IωL = I\omega
  • Analogous to p=mvp = mv.
K.E.=12Iω2=12Lω=L22I\text{K.E.} = \dfrac{1}{2}I\omega^2 = \dfrac{1}{2}L\omega = \dfrac{L^2}{2I}—

Torque in Terms of Moment of Inertia

FormulaSymbols, units and conditions
τ⃗=r⃗×F⃗,τ=Iα,τ⃗=dL⃗dt\vec\tau = \vec r\times\vec F, \qquad \tau = I\alpha, \qquad \vec\tau = \dfrac{d\vec L}{dt}
  • SI unit N m; dimensions [M1L2T−2][M^1L^2T^{-2}]. Analogous to f=maf = ma and f=dpdtf = \dfrac{dp}{dt}.
τ=I(ω2−ω1t),W=τθ,P=τω=2πnτ\tau = I\left(\dfrac{\omega_2-\omega_1}{t}\right), \qquad W = \tau\theta, \qquad P = \tau\omega = 2\pi n\tau
  • Average torque, work done by a torque, and power. PP in watt when τ\tau is in N m and ω\omega in rad/s.

Conservation of Angular Momentum

FormulaSymbols, units and conditions
If τ⃗ext=0,dL⃗dt=0⇒L⃗=Iω⃗=constant\text{If } \vec\tau_{ext}=0, \quad \dfrac{d\vec L}{dt}=0 \quad \Rightarrow \quad \vec L = I\vec\omega = \text{constant}—
I1ω1=I2ω2,I1n1=I2n2I_1\omega_1 = I_2\omega_2, \qquad I_1 n_1 = I_2 n_2
  • Used whenever mass redistributes about the axis (blob of wax on a disc, a leaking balloon, a diver folding up).
I2=I1+mr2I_2 = I_1 + mr^2
  • Moment of inertia after a particle of mass mm sticks at a distance rr from the axis (parallel axes / point-mass addition).

Rolling Motion

FormulaSymbols, units and conditions
v=Rωv = R\omega
  • Rolling without slipping; vv = speed of the centre of mass, RR = radius of the rolling body.
E=12Mv2+12Iω2=12Mv2[1+K2R2]E = \dfrac{1}{2}Mv^2 + \dfrac{1}{2}I\omega^2 = \dfrac{1}{2}Mv^2\left[1+\dfrac{K^2}{R^2}\right]
  • Total kinetic energy of a rolling body = translational + rotational.
v=2gh1+K2R2,a=gsin⁡θ1+K2R2v = \sqrt{\dfrac{2gh}{1+\dfrac{K^2}{R^2}}}, \qquad a = \dfrac{g\sin\theta}{1+\dfrac{K^2}{R^2}}
  • Rolling without slipping down an incline of inclination θ\theta, through a vertical height hh; distance along the incline s=hsin⁡θs = \dfrac{h}{\sin\theta}. For pure sliding (frictionless) the same expressions hold with K2R2=0\dfrac{K^2}{R^2}=0.
  • BodyK2R2\dfrac{K^2}{R^2}Trans. : Rot. : Total K.E.
  • Ring, hollow cylinder111:1:21:1:2
  • Uniform disc, solid cylinder12\dfrac{1}{2}2:1:32:1:3
  • Thin walled hollow sphere23\dfrac{2}{3}3:2:53:2:5
  • Solid sphere25\dfrac{2}{5}5:2:75:2:7
  • If I=n(MR2)I = n\left(MR^2\right), then the numerical factor nn is exactly K2R2\dfrac{K^2}{R^2}. The ratio Translational : Rotational : Total K.E. is 1:K2R2:(1+K2R2)1:\dfrac{K^2}{R^2}:\left(1+\dfrac{K^2}{R^2}\right).

Standard Values Used in Board Numericals

  • g=10g = 10 m/s2^2 in textbook problems unless otherwise stated; g=9.8g = 9.8 m/s2^2 wherever the paper states it.
  • π=3.142\pi = 3.142 (or 3.143.14); some problems set π2=10\pi^2 = 10.
  • 11 km/h =518= \dfrac{5}{18} m/s. 11 rpm =160= \dfrac{1}{60} rps.
Short NotesThe chapter subtopic by subtopic, in the textbook's own order.11 subtopics
  1. 1Introduction
  2. 2Characteristics of Circular Motion14 board questions
  3. 3Applications of Uniform Circular Motion18 board questions
  4. 4Vertical Circular Motion6 board questions
  5. 5Moment of Inertia as an Analogous Quantity for Mass3 board questions
  6. 6Radius of Gyration3 board questions
  7. 7Theorem of Parallel Axes and Theorem of Perpendicular Axes13 board questions
  8. 8Angular Momentum or Moment of Linear Momentum2 board questions
  9. 9Expression for Torque in Terms of Moment of Inertia8 board questions
  10. 10Conservation of Angular Momentum6 board questions
  11. 11Rolling Motion3 board questions
The whole chapter in brief

1.1 Introduction

  • Revolution: every particle of the object moves in a circle about a point outside the object, or about another object.
  • Rotation: the motion is about an axis of rotation that passes through the object itself.

1.2 Characteristics of Circular Motion

  • It is an accelerated motion — the direction of velocity changes at every instant, even when the speed is constant.
  • It is a periodic motion — the particle repeats the same path, so the motion is periodic in space.
  • Uniform circular motion (U.C.M.): circular motion in which the speed of the particle remains constant. Only the direction of v⃗\vec v changes, and v⃗\vec v is always tangential.
  • Non-uniform circular motion: the speed changes as well, so both a⃗r\vec a_r (magnitude no longer constant) and a⃗T\vec a_T are present.
  • Tangential acceleration in U.C.M. is always zero.
  • v⃗=ω⃗×r⃗\vec v = \vec\omega\times\vec r; ω⃗\vec\omega and α⃗\vec\alpha lie along the axis of rotation, direction given by the right-hand thumb rule (curl the fingers along the sense of rotation, the outstretched thumb gives ω⃗\vec\omega).
  • For increasing speed α⃗\vec\alpha is along ω⃗\vec\omega; for decreasing speed it is opposite to ω⃗\vec\omega.
  • If α⃗\vec\alpha has a component perpendicular to the axis, it changes the direction of ω⃗\vec\omega and hence the plane of rotation. If α⃗\vec\alpha is constant in magnitude but always perpendicular to ω⃗\vec\omega, it changes only the direction of ω⃗\vec\omega and never its magnitude.
  • Kinematical equations ω=ω0+αt\omega=\omega_0+\alpha t, θ=ω0t+12αt2\theta=\omega_0t+\dfrac{1}{2}\alpha t^2, ω2=ω02+2αθ\omega^2=\omega_0^2+2\alpha\theta hold only for constant, axial α\alpha.

Centripetal and centrifugal force

  • Centripetal force is the resultant of all the real forces acting on the body, directed towards the centre: F⃗CP=−mω2r⃗\vec F_{CP}=-m\omega^2\vec r, FCP=mrω2=mv2r=mvωF_{CP}=mr\omega^2=\dfrac{mv^2}{r}=mv\omega.
  • "Centripetal" is not the name or type of a force — it is an adjective describing its direction (centre-seeking). The force itself is gravity, tension, friction or normal reaction.
  • The converse is not true: a force directed towards a centre need not produce circular motion (S.H.M. is a counter-example). A matching tangential velocity is also essential.
  • Centrifugal force is the net pseudo force in the rotating (non-inertial) frame: F⃗CF=+mω2r⃗\vec F_{CF}=+m\omega^2\vec r. It is non-real, but not imaginary — an instrument in that frame records it.
  • Only in the frame of the rotating body can we say that centrifugal force balances centripetal force; there the resultant is zero.
Centripetal forceCentrifugal force
Directed along the radius, towards the centreDirected along the radius, away from the centre
It is a real forceIt is a pseudo force
Considered in an inertial frame of referenceConsidered in a non-inertial frame of reference
F⃗=−mv2rr^0\vec F = -\dfrac{mv^2}{r}\hat r_0F⃗=+mv2rr^0\vec F = +\dfrac{mv^2}{r}\hat r_0

1.3 Applications of Uniform Circular Motion

Vehicle on a horizontal circular track

  • Forces: weight mgmg down, normal reaction NN up (N=mgN=mg), and static friction fsf_s towards the centre. Friction is static because it prevents outward slipping (skidding).
  • fsN=v2rg\dfrac{f_s}{N}=\dfrac{v^2}{rg}, and since fs≤μsNf_s \le \mu_s N, the speed has an upper limit vmax=μsrgv_{max}=\sqrt{\mu_s rg} — independent of the mass.
  • A two-wheeler rider must lean at θ=tan⁡−1 ⁣(v2rg)\theta = \tan^{-1}\!\left(\dfrac{v^2}{rg}\right) with the vertical so that the torque of the weight balances the torque of the centrifugal and frictional forces. A four-wheeler does not lean because its four normal reactions (unequal during a turn) already supply the balancing torque.

Well (wall) of death

  • Vertical cylindrical wall of radius rr. Normal reaction NN is horizontal and is the entire centripetal force; static friction fsf_s acts vertically upwards and equals mgmg (the only upward force).
  • fs≤μsNf_s \le \mu_s N gives a lower limit: vmin=rgμsv_{min}=\sqrt{\dfrac{rg}{\mu_s}}. The largest allowed period is Tmax=2πrvminT_{max}=\dfrac{2\pi r}{v_{min}}.
  • fs=μsNf_s=\mu_s N holds only at the minimum speed; at all higher speeds fsf_s is still exactly mgmg.
  • Banking angle here is 90∘90^\circ, which is why it imposes a lower limit. For 0<θ<90∘0<\theta<90^\circ there are both an upper and a lower limit.

Vehicle on a banked road

  • Roads are banked so that the horizontal component of the normal reaction supplies the centripetal force and we need not depend on friction, whose value is limited and not uniform over a road surface.
  • Frictionless analysis: Ncos⁡θ=mgN\cos\theta = mg, Nsin⁡θ=mv2rN\sin\theta = \dfrac{mv^2}{r}, hence tan⁡θ=v2rg\tan\theta = \dfrac{v^2}{rg} and vs=rgtan⁡θv_s=\sqrt{rg\tan\theta} — the most safe speed, not a maximum or minimum, and independent of the mass.
  • Below vsv_s, friction acts up the incline; above vsv_s, it acts down the incline.
  • vmin=rg(tan⁡θ−μs1+μstan⁡θ)v_{min}=\sqrt{rg\left(\dfrac{\tan\theta-\mu_s}{1+\mu_s\tan\theta}\right)} and vmax=rg(tan⁡θ+μs1−μstan⁡θ)v_{max}=\sqrt{rg\left(\dfrac{\tan\theta+\mu_s}{1-\mu_s\tan\theta}\right)}.
  • If μs≥tan⁡θ\mu_s \ge \tan\theta then vmin=0v_{min}=0 (true for most rough roads banked at small angles). If μs=cot⁡θ\mu_s=\cot\theta then vmax→∞v_{max}\to\infty; since (μs)max=1(\mu_s)_{max}=1, this means no upper limit for θ≥45∘\theta\ge 45^\circ.
  • Even a two-wheeler benefits from banking — it then needs to lean less, and the same limits apply.
  • If friction were zero the vehicle could still move at exactly vsv_s, but at any other speed it would skid; so the honest board answer is "No, the vehicle will skid in the absence of friction."

Conical pendulum

  • A bob revolving in a horizontal circle so that the string sweeps out a right circular cone of vertical axis.
  • T0cos⁡θ=mgT_0\cos\theta = mg (balances the weight), T0sin⁡θ=mv2r=mrω2T_0\sin\theta = \dfrac{mv^2}{r} = mr\omega^2 (the centripetal force). Dividing, tan⁡θ=v2rg\tan\theta = \dfrac{v^2}{rg}.
  • With r=Lsin⁡θr=L\sin\theta: ω=gLcos⁡θ\omega=\sqrt{\dfrac{g}{L\cos\theta}}, period T=2πLcos⁡θgT=2\pi\sqrt{\dfrac{L\cos\theta}{g}}, frequency n=12πgLcos⁡θn=\dfrac{1}{2\pi}\sqrt{\dfrac{g}{L\cos\theta}}.
  • Period and frequency depend on LL, gg and θ\theta — never on the mass of the bob.
  • The string can never become horizontal: at θ=90∘\theta=90^\circ the vertical component of tension vanishes and nothing balances mgmg; also T0=mgcos⁡θT_0=\dfrac{mg}{\cos\theta}, the kinetic energy and the frequency would all become infinite and the period zero.

1.4 Vertical Circular Motion

  • Two kinds: (a) controlled, such as a giant wheel, where the speed is not governed by gravity alone; (b) controlled only by gravity, where energy is supplied once at the lowest point and thereafter K.E. and gravitational P.E. interconvert.
  • Only two forces act at any position: constant weight mgmg, and the force due to tension TT (or normal reaction NN) along the string towards the centre.
  • The resultant is purely centripetal only at the uppermost and lowermost points. Elsewhere part of it is tangential and changes the speed.
PositionForce equationMinimum speed
Uppermost, Amg+TA=mvA2rmg+T_A=\dfrac{mv_A^2}{r}rg\sqrt{rg}
Midway (string horizontal), C or DTC=mvC2rT_C=\dfrac{mv_C^2}{r}3rg\sqrt{3rg}
Lowermost, BTB−mg=mvB2rT_B-mg=\dfrac{mv_B^2}{r}5rg\sqrt{5rg}
  • Energy conservation over the drop 2r2r gives vB2−vA2=4rgv_B^2-v_A^2=4rg; over the drop rr, vB2−vC2=2rgv_B^2-v_C^2=2rg.
  • TB−TA=6mgT_B-T_A=6mg and TC−TA=3mgT_C-T_A=3mg. These are independent of vv and rr — they depend only on the weight.
  • TAT_A can never be exactly zero for a string (it would slacken), so in practice TB>6mgT_B>6mg.
  • At an arbitrary angle θ\theta from the lowest point, T=mv2r+mgcos⁡θT=\dfrac{mv^2}{r}+mg\cos\theta, and the rise above the lowest point is r(1−cos⁡θ)r(1-\cos\theta).
  • Rod instead of string: the rod can push as well as pull, so zero speed is possible at the top. Then (vlowermost)min=4rg(v_{lowermost})_{min}=\sqrt{4rg}, (vmidway)min=2rg(v_{midway})_{min}=\sqrt{2rg}, and still Tlowermost−Tuppermost=6mgT_{lowermost}-T_{uppermost}=6mg.
  • Sphere of death: identical dynamics with NN in place of TT.
  • Convex over-bridge: mg−N=mv2rmg-N=\dfrac{mv^2}{r}; NN falls as vv rises and contact is just lost at vmax=rgv_{max}=\sqrt{rg}.
  • No parameter is constant in this motion, so the kinematical equations of Table 1 do not apply, and the period cannot be found theoretically (only measured).

1.5 Moment of Inertia

  • Definition: the moment of inertia of a rigid body about an axis of rotation is the sum of the products of the mass of each particle and the square of its perpendicular distance from that axis.
  • I=∑miri2=∫r2 dmI=\sum m_i r_i^2 = \int r^2\,dm. SI unit kg m2^2; dimensions [M1L2T0][M^1L^2T^0].
  • It depends on (i) the individual masses and (ii) how those masses are distributed about the given axis — so the same body has different II about different axes.
  • Rotational K.E. =12Iω2=\dfrac{1}{2}I\omega^2, the exact analogue of 12mv2\dfrac{1}{2}mv^2; this is what identifies II as the rotational analogue of mass.
  • Uniform ring about its own axis: the whole mass is at distance RR, so I=MR2I=MR^2 with no integration.
  • Uniform disc about its own axis: integrating over concentric rings, I=12MR2I=\dfrac{1}{2}MR^2.

1.6 Radius of Gyration

  • Definition: the distance between the axis of rotation and the point at which the whole mass of the body may be supposed to be concentrated so as to give the same moment of inertia about that axis. I=MK2I=MK^2.
  • Its use: II can be calculated only for mathematically integrable shapes, but it can be measured for any object. Writing I=MK2I=MK^2 separates out the mass and leaves KK carrying the information about how the mass is distributed.
  • KK depends on the distribution of mass about the given axis (and on the shape and the choice of axis); it does not depend on the mass of the body.
  • Larger KK means the mass sits farther from the axis. For the same MM and RR: Kring=RK_{ring}=R, Kdisc=R2K_{disc}=\dfrac{R}{\sqrt2}, so Kd<KrK_d<K_r — among objects of the same mass and radius, the ring has the largest KK and hence the largest II.
  • Like the centre of mass, KK is a single equivalent location that stands in for the whole distribution — but it is defined with respect to an axis, not a point.

1.7 Theorems of Parallel and Perpendicular Axes

Theorem of parallel axesTheorem of perpendicular axes
IO=IC+Mh2I_O=I_C+Mh^2Iz=Ix+IyI_z=I_x+I_y
Needs two parallel axes, one passing through the centre of massNeeds three mutually perpendicular concurrent axes
Applies to any object, laminar or notApplies only to a laminar (two-dimensional) object
hh = distance between the axesxx and yy lie in the plane, zz is perpendicular to it
  • In terms of radius of gyration, the parallel axes theorem reads KO2=KC2+h2K_O^2=K_C^2+h^2.
  • Useful transforms: disc about a diameter 14MR2\dfrac{1}{4}MR^2; disc about a tangent in its plane 54MR2\dfrac{5}{4}MR^2; disc about a tangent perpendicular to its plane 32MR2\dfrac{3}{2}MR^2; ring about a diameter 12MR2\dfrac{1}{2}MR^2; sphere about a tangent 75MR2\dfrac{7}{5}MR^2; rod about a transverse axis through one end 13ML2\dfrac{1}{3}ML^2.

1.8 Angular Momentum

  • L⃗=r⃗×p⃗\vec L=\vec r\times\vec p; in magnitude L=prsin⁡θL=pr\sin\theta, the product of linear momentum and its perpendicular distance from the axis.
  • For a rigid body rotating about a fixed axis, L=IωL=I\omega — analogous to p=mvp=mv, which is the physical significance of II.
  • K.E. =12Iω2=12Lω=L22I=\dfrac{1}{2}I\omega^2=\dfrac{1}{2}L\omega=\dfrac{L^2}{2I}.
  • SI unit kg m2^2/s; dimensions [M1L2T−1][M^1L^2T^{-1}].

1.9 Torque

  • τ=Iα\tau = I\alpha, obtained by summing miri2αm_i r_i^2\alpha over all particles — analogous to f=maf=ma.
  • τ⃗=r⃗×F⃗=dL⃗dt\vec\tau=\vec r\times\vec F=\dfrac{d\vec L}{dt}. SI unit N m; dimensions [M1L2T−2][M^1L^2T^{-2}].
  • Work done by a torque W=τθW=\tau\theta; power P=τω=2πnτP=\tau\omega=2\pi n\tau.
  • A "couple of 20 N m" in a numerical simply means a torque of 20 N m.

1.10 Conservation of Angular Momentum

  • Statement: the angular momentum of an isolated system is conserved in the absence of an external unbalanced torque.
  • Proof in one line: dL⃗dt=r⃗×F⃗+m(v⃗×v⃗)=τ⃗\dfrac{d\vec L}{dt}=\vec r\times\vec F+m(\vec v\times\vec v)=\vec\tau, and v⃗×v⃗=0\vec v\times\vec v=0; so τ⃗=0\vec\tau=0 gives L⃗\vec L = constant.
  • Working form: I1ω1=I2ω2I_1\omega_1=I_2\omega_2, i.e. I1n1=I2n2I_1n_1=I_2n_2. Decreasing II raises nn and vice versa.
  • Standard examples: ballet dancers and ice skaters pulling limbs in for fast small-radius rounds and stretching out for slow large-radius ones; a diver folding up after leaving the board to spin faster and stretching out for a clean entry; a planet speeding up near the sun in an elliptical orbit; a person on a rotating platform changing speed by moving weights in and out.
  • For a planet in a circular orbit the angular momentum is trivially constant too — conservation applies to both circular and elliptical orbits, because the gravitational force is central and exerts no torque about the sun.

1.11 Rolling Motion

  • Pure rolling is treated as rotation of the whole body about its own symmetry axis plus translation of the whole mass concentrated at the centre of mass; the centre of mass performs purely translational motion, and v=Rωv=R\omega.
  • Static friction is essential for pure rolling — it prevents sliding. It is why a pushed sphere first slips and only then starts rolling.
  • E=12Mv2+12Iω2=12Mv2[1+K2R2]E=\dfrac{1}{2}Mv^2+\dfrac{1}{2}I\omega^2=\dfrac{1}{2}Mv^2\left[1+\dfrac{K^2}{R^2}\right].
  • Down an incline: v=2gh1+K2R2v=\sqrt{\dfrac{2gh}{1+\dfrac{K^2}{R^2}}} and a=gsin⁡θ1+K2R2a=\dfrac{g\sin\theta}{1+\dfrac{K^2}{R^2}}. For pure sliding these become 2gh\sqrt{2gh} and gsin⁡θg\sin\theta — the factor (1+K2R2)\left(1+\dfrac{K^2}{R^2}\right) is the only difference.
  • Because K2R2\dfrac{K^2}{R^2} contains no mass and no radius, all bodies of the same shape roll down an incline with the same acceleration, whatever their size or mass.
  • When a rod rolls, it is really a cylinder that is rolling.

Analogy Between Translational and Rotational Motion

TranslationalRotationalRelation
Displacement s⃗\vec sAngular displacement θ⃗\vec\thetas⃗=θ⃗×r⃗\vec s=\vec\theta\times\vec r
Velocity v⃗=ds⃗dt\vec v = \dfrac{d\vec s}{dt}Angular velocity ω⃗=dθ⃗dt\vec\omega=\dfrac{d\vec\theta}{dt}v⃗=ω⃗×r⃗\vec v=\vec\omega\times\vec r
Acceleration a⃗=dv⃗dt\vec a=\dfrac{d\vec v}{dt}Angular acceleration α⃗=dω⃗dt\vec\alpha=\dfrac{d\vec\omega}{dt}a⃗=α⃗×r⃗\vec a=\vec\alpha\times\vec r
Mass mmMoment of inertia III=∫r2dmI=\int r^2 dm
Linear momentum p⃗=mv⃗\vec p=m\vec vAngular momentum L⃗=Iω⃗\vec L=I\vec\omegaL⃗=r⃗×p⃗\vec L=\vec r\times\vec p
Force f⃗=dp⃗dt\vec f=\dfrac{d\vec p}{dt}Torque τ⃗=dL⃗dt\vec\tau=\dfrac{d\vec L}{dt}τ⃗=r⃗×f⃗\vec\tau=\vec r\times\vec f
Work W=f⃗⋅s⃗W=\vec f\cdot\vec sWork W=τ⃗⋅θ⃗W=\vec\tau\cdot\vec\theta—
Power P=f⃗⋅v⃗P=\vec f\cdot\vec vPower P=τ⃗⋅ω⃗P=\vec\tau\cdot\vec\omega—
K.E. =12mv2=\dfrac{1}{2}mv^2K.E. =12Iω2=\dfrac{1}{2}I\omega^2—

Traps That Cost Marks

  • Writing "centripetal force" as a separate extra force in a free-body diagram. It is the resultant of the real forces already drawn, not another arrow.
  • Forgetting that ω⃗\vec\omega points along the axis, not along the velocity. A fan seen from below turning anticlockwise and slowing has ω⃗\vec\omega upwards (towards the viewer, downwards in space terms is the common error) and α⃗\vec\alpha opposite to ω⃗\vec\omega.
  • Converting rpm carelessly. Always n(rps)=n(rpm)60n(\text{rps})=\dfrac{n(\text{rpm})}{60}, then ω=2πn\omega=2\pi n. For angular displacement, NN revolutions is 2πN2\pi N rad.
  • Quoting vmin=μsrgv_{min}=\sqrt{\mu_s rg} for the well of death. There it is vmin=rgμsv_{min}=\sqrt{\dfrac{rg}{\mu_s}} — the μs\mu_s moves to the denominator.
  • Using 5rg\sqrt{5rg} at the top of a vertical circle. rg\sqrt{rg} is the top, 3rg\sqrt{3rg} the midway point, 5rg\sqrt{5rg} the bottom.
  • Applying the perpendicular axes theorem to a solid sphere or a cylinder. It works only for laminar objects.
  • Applying the parallel axes theorem from an axis that is not through the centre of mass. ICI_C in IO=IC+Mh2I_O=I_C+Mh^2 must be about the centre-of-mass axis.
  • Using 12Mv2\dfrac{1}{2}Mv^2 alone for a rolling body. The rotational share is K2R2\dfrac{K^2}{R^2} times the translational share.
  • Mixing up 112ML2\dfrac{1}{12}ML^2 (rod about its centre) with 13ML2\dfrac{1}{3}ML^2 (rod about one end).
  • Leaving the answer in cm, g or rpm when the question asks for SI units.

Two Quick Results Worth Memorising

  • A uniform disc and a uniform hollow right circular cone have the same central-axis formula 12MR2\dfrac{1}{2}MR^2 — because in both, the mass per unit radial distance is distributed in the same proportional way about the axis.
  • If a disc has K=2.5K=\sqrt{2.5} about its central transverse axis, then R22=2.5\dfrac{R^2}{2}=2.5, so R2=5R^2=5; about a tangent in its plane I=54MR2I=\dfrac{5}{4}MR^2 gives K2=6.25K^2=6.25, i.e. K=2.5K=2.5 in the same units.
Solved Numerical ExamplesWorked numericals to attempt first, each with a hint before the full solution.Coming soon

These are being added chapter by chapter. They are solved numericals from the prescribed book and the reference guides — not previous board questions, which live under Practice — so that you can work through the method before meeting it in a real paper.

Important DerivationsEvery derive / obtain / prove question in this chapter. 4 have come up in two or more papers.14
  1. 1
    Kinetic energy of a rotating body (uniform angular speed) Repeats
    Derive an expression for the kinetic energy of a body rotating with a uniform angular speed.

    Asked in: March 2022 (Q.19, 3 marks); July 2022 (Q.17, 3 marks)

    Show the derivation
    Derivation of an expression for the kinetic energy of a body rotating with a uniform angular speed:
    Step 1
    Consider a rigid object rotating with a constant angular speed ω about an axis perpendicular to the plane of paper.
    Step 2
    For theoretical simplification, let us consider the object to be consisting of N particles of masses m1,m2,....mNm_1, m_2,....m_N at respective perpendicular distances r1,r2,....rNr_1, r_2,....r_N from the axis of rotation.
    Step 3
    As the object rotates, all these particles perform UCM with the same angular speed ω, but with different linear speeds, v1=r1ω,v2=r2ω,....,vN=rNωv_1=r_1\omega, v_2=r_2\omega,....,v_N=r_N\omega
    Step 4
    Translational K.E. of the first particle is, (K.E.)1=12m1v12=12m1r12ω2(K.E.)_1 = \dfrac{1}{2}m_1v_1^2 = \dfrac{1}{2}m_1r_1^2\omega^2
    Translational K.E. of the second particle is, (K.E.)2=12m2v22=12m2r22ω2(K.E.)_2 = \dfrac{1}{2}m_2v_2^2 = \dfrac{1}{2}m_2r_2^2\omega^2
    Similar will be the case of all the remaining particles.
    Step 5
    Rotational K.E. of the object is the sum of individual translational kinetic energies. Thus,
    Rotational K.E.=12m1r12ω2+12m2r22ω2....+12mNrN2ω2\text{Rotational K.E.} = \dfrac{1}{2}m_1r_1^2\omega^2+\dfrac{1}{2}m_2r_2^2\omega^2....+\dfrac{1}{2}m_Nr_N^2\omega^2
    ∴Rotational K.E.=12(m1r12+m2r22....+mNrN2)ω2\therefore \text{Rotational K.E.} = \dfrac{1}{2}(m_1r_1^2+m_2r_2^2....+m_Nr_N^2)\omega^2
    But I=∑i=1Nmiri2=m1r12+m2r22....+mNrN2\text{But } I=\sum_{i=1}^{N}m_ir_i^2 = m_1r_1^2+m_2r_2^2....+m_Nr_N^2
    ∴\therefore Rotational K.E. =12Iω2=\dfrac{1}{2}I\omega^2
  2. 2
    Principle of conservation of angular momentum Repeats
    State and prove the principle of conservation of angular momentum.

    Asked in: October 2015; February 2023 (Q.5, 2 marks)

    Show the derivation
    Step 1
    Statement: Angular momentum of an isolated system is conserved in the absence of an external unbalanced torque.
    Step 2
    Illustration — Ballet dancers: a. During ice ballet, the dancers have to undertake rounds of smaller and larger radii. b. The dancers come together by taking rounds of smaller radius (near the centre). c. In this case, the moment of inertia of their system becomes minimum and the frequency increases, to make it thrilling. d. While during outer rounds, the dancers outstretch their legs and arms. e. This increases their moment of inertia that reduces the angular speed and hence the linear speed. This is essential to prevent slipping.
    Proof
    Step 1
    Angular momentum or the moment of linear momentum of a system is given by, L⃗=r⃗×p⃗\vec L=\vec r\times\vec p
    where r⃗\vec r is the position vector from the axis of rotation and p⃗\vec p is the linear momentum.
    Step 2
    Differentiating with respect to time, we get,
    dL⃗dt=ddt(r⃗×p⃗)=r⃗×dp⃗dt+dr⃗dt×p⃗\dfrac{d\vec L}{dt}=\dfrac{d}{dt}(\vec r\times\vec p)=\vec r\times\dfrac{d\vec p}{dt}+\dfrac{d\vec r}{dt}\times\vec p
    Step 3
    Now, dr⃗dt=v⃗\dfrac{d\vec r}{dt}=\vec v and dp⃗dt=F⃗\dfrac{d\vec p}{dt}=\vec F
    ∴dL⃗dt=r⃗×F⃗+m(v⃗×v⃗)\therefore \dfrac{d\vec L}{dt}=\vec r\times\vec F+m(\vec v\times\vec v)
    Now (v⃗×v⃗)=0(\vec v\times\vec v)=0
    ∴dL⃗dt=r⃗×F⃗\therefore \dfrac{d\vec L}{dt}=\vec r\times\vec F
    Step 4
    But r⃗×F⃗\vec r\times\vec F is the moment of force or torque τ⃗\vec\tau.
    ∴τ⃗=dL⃗dt\therefore \vec\tau=\dfrac{d\vec L}{dt}
    Thus, if τ⃗=0\vec\tau=0, dL⃗dt=0\dfrac{d\vec L}{dt}=0 or L⃗=\vec L= constant.
    Hence, angular momentum L⃗\vec L is conserved in the absence of external unbalanced torque τ⃗\vec\tau.
  3. 3
    Theorem of parallel axes Repeats
    State and prove the theorem of parallel axes.

    Asked in: March 2014; July 2023 (Q.27, 4 marks)

    Show the derivation
    StatementThe moment of inertia (IOI_O) of an object about any axis is the sum of its moment of inertia (ICI_C) about an axis parallel to the given axis, and passing through the centre of mass and the product of the mass of the object and the square of the distance between the two axes.
    Mathematically, IO=IC+Mh2I_O = I_C+Mh^2
    Proof
    Step 1
    Consider an object of mass M. Axis MOP is any axis passing through point O.
    Step 2
    Axis ACB is passing through the centre of mass C of the object, parallel to the axis MOP, and at a distance h from it (∴h=CO\therefore h = CO).
    Step 3
    Consider a mass element 'dm' located at point D. Perpendicular on OC (produced) from point D is DN.
    Step 4
    Moment of inertia of the object about the axis ACB is Ic=∫(DC)2dmI_c=\int(DC)^2dm, and about the axis MOP it is Io=∫(DO)2dmI_o=\int(DO)^2dm.
    ∴Io=∫(DO)2dm=∫[(DN)2+(NO)2]dm\therefore I_o=\int(DO)^2dm=\int\left[(DN)^2+(NO)^2\right]dm
    =∫[(DN)2+(NC)2+2⋅NC⋅CO+(CO)2]dm=\int\left[(DN)^2+(NC)^2+2\cdot NC\cdot CO+(CO)^2\right]dm
    =∫[(DC)2+2NC⋅h+h2]dm....(using Pythagoras theorem in △DNC)=\int\left[(DC)^2+2NC\cdot h+h^2\right]dm\qquad....(\text{using Pythagoras theorem in }\triangle DNC)
    =∫(DC)2dm+2h∫NC⋅dm+h2∫dm=\int(DC)^2dm+2h\int NC\cdot dm+h^2\int dm
    Now, ∫(DC)2dm=Ic\int(DC)^2dm = I_c and ∫dm=M\int dm = M
    Step 5
    NC is the distance of a point from the centre of mass. Any mass distribution is symmetric about the centre of mass. Thus, from the definition of the centre of mass, ∫NC⋅dm=0\int NC\cdot dm = 0
    ∴Io=Ic+Mh2\therefore I_o = I_c+Mh^2
    This is the mathematical form of the theorem of parallel axes.
  4. 4
    Maximum speed of a vehicle on a horizontal circular track
    Derive an expression for maximum speed of a vehicle moving along a horizontal circular track.

    Asked in: February 2024 (Q.11, 2 marks)

    Show the derivation
    Step 1
    Consider vertical section of a car moving on a horizontal circular track having a radius 'r' with 'C' as centre of track.
    Step 2
    Forces acting on the car (considered to be a particle): (a) Weight (mg), vertically downwards, (b) Normal reaction (N), vertically upwards that balances the weight, (c) Force of static friction (fsf_s) between road and the tyres.
    Step 3
    Since, normal reaction balances the weight
    ∴N=mg\therefore N = mg ....(1)
    Step 4
    The friction over here is static friction which acts as resultant centripetal force because it prevents the vehicle from outward slipping or skidding.
    Step 5
    While working in the frame of reference attached to the vehicle, the frictional force balances the centrifugal force.
    fs=mv2r....(2)f_s = \dfrac{mv^2}{r}\qquad....(2)
    Dividing equation (2) by equation (1),
    fsN=v2rg....(3)\dfrac{f_s}{N} = \dfrac{v^2}{rg}\qquad....(3)
    Step 6
    For a given track, radius r is constant. For given vehicle, mg = N is constant. Thus, as the speed v increases, the force of static friction fsf_s also increases.
    Step 7
    However, fsf_s has an upper limit (fs)max=μsN(f_s)_{max} = \mu_sN, where μs\mu_s is the coefficient of static friction between road and tyres of the vehicle. This imposes an upper limit to the speed v.
    Step 8
    At the maximum possible speed,
    (fs)maxN=μs=vmax2rg....[From equations (2) and (3)]\dfrac{(f_s)_{max}}{N} = \mu_s = \dfrac{v_{max}^2}{rg}\qquad....[\text{From equations (2) and (3)}]
    ∴vmax=μsrg\therefore v_{max} = \sqrt{\mu_srg}
    This is an expression for maximum possible speed for a vehicle to move on a horizontal circular track.
  5. 5
    Vertical circular motion -- velocities at lowest, mid-way and top-most positions
    Derive expressions for linear velocity at the lowest position, mid-way position and the top-most position for a particle revolving in a vertical circle, if it has to just complete the circular motion without the string slackening at the top.

    Asked in: February 2023 (Q.31, 4 marks)

    Show the derivation
    [From 1.4, Q1 (i)]
    Step 1
    Consider a particle of mass m moving along a vertical circle.
    Step 2
    At any position of the particle, there are only two forces acting on the particle: a. weight (mg), vertically downwards, which is constant; b. the force due to the tension (T), directed towards the centre. (Its magnitude changes periodically with time and location.)
    Step 3
    As the motion is non uniform, the resultant of these two forces is not directed towards the centre except at the uppermost and the lowermost positions of the bob.
    Step 4
    Uppermost position (A): a. Both, weight (mg) and force due to tension (TAT_A) are downwards, i.e., towards the centre. In this case, their resultant is used only as the centripetal force. b. Thus, if vAv_A is the speed at the uppermost point,
    mg+TA=mvA2r....(1)mg + T_A = \dfrac{mv_A^2}{r}\qquad....(1)
    c. For minimum possible speed at this point (or if the motion is to be realized with minimum possible energy), TA=0T_A = 0
    ∴(vA)min=rg....(2)\therefore (v_A)_{min} = \sqrt{rg}\qquad....(2)
    Step 5
    Lowermost position (B): a. Force due to the tension, TBT_B is vertically upwards, i.e., towards the centre, and opposite to mg. In this case, their resultant is the centripetal force. b. If vBv_B is the speed at the lowermost point,
    TB−mg=mvB2r....(3)T_B - mg = \dfrac{mv_B^2}{r}\qquad....(3)
    c. While coming down from the uppermost to the lowermost point, the vertical displacement is 2r and the motion is governed only by gravity. d. Hence the corresponding decrease in the gravitational potential energy is converted into the kinetic energy.
    ∴mg(2r)=12mvB2−12mvA2\therefore mg(2r) = \dfrac{1}{2}mv_B^2-\dfrac{1}{2}mv_A^2
    ∴vB2−vA2=4rg....(4)\therefore v_B^2-v_A^2 = 4rg\qquad....(4)
    Step 6
    Difference between the extreme tensions: Subtracting equation (1) from equation (3),
    TB−TA−2mg=mr(vB2−vA2)....(5)T_B-T_A-2mg = \dfrac{m}{r}(v_B^2-v_A^2)\qquad....(5)
    Using equation (4) and rearranging, we get,
    ∴TB−TA=6mg\therefore T_B-T_A = 6mg
    Hence, difference in tension at extreme positions depends only on weight. to (v) and diagram.
    vi. Positions when the string is horizontal (C and D): a. Force due to the tension is the only force towards the centre as weight mg is perpendicular to the tension. b. Thus, force due to the tension is the centripetal force used to change the direction of the velocity and weight mg is used only to change the speed. c. At midway position (C), while coming down from the midway point to the lowermost point, the vertical displacement is 'r'. Hence, the corresponding decrease in the gravitational P.E. is converted into K.E.
    mgr=12mvA2−12mvC2mgr = \dfrac{1}{2}mv_A^2-\dfrac{1}{2}mv_C^2
    ∴vA2−vC2=2gr\therefore v_A^2-v_C^2 = 2gr
    Since, vA=5rgv_A = \sqrt{5rg}
    ∴vC2=5rg−2rg\therefore v_C^2 = 5rg-2rg
    ∴(vC)min=3rg\therefore (v_C)_{min} = \sqrt{3rg}
    Similarly (vD)min=3rg(v_D)_{min} = \sqrt{3rg}
  6. 6
    Minimum speed to perform stunts in a 'well of death'
    Derive an expression for minimum speed to perform stunts in a well of death.

    Asked in: July 2024 (Q.27, 4 marks)

    Show the derivation

    The question is a real board question. This working is ours — no source printed a derivation for it.

    Diagram

    Draw a vertical cylinder of inner radius rr seen from the side, with the motorcycle on the inside of the wall at the level of the centre. Mark three forces at the point of contact: the normal reaction NN pointing horizontally inwards, towards the axis of the cylinder; the weight mgmg vertically downwards; and the force of static friction fsf_s vertically upwards along the wall.

    Setting up

    The rider moves in a horizontal circle of radius rr on the inside of the vertical wall, so the centripetal force must be horizontal and directed at the axis. The only horizontal force acting is the normal reaction, so

    N=mv2rN = \dfrac{mv^{2}}{r}

    The wall is vertical, so it can hold the rider up only through friction. For the rider not to slide down, the upward force of static friction must balance the weight:

    fs=mgf_s = mg

    Applying the limit on static friction

    Static friction cannot exceed its limiting value,

    fs≤μsNf_s \le \mu_s N

    where μs\mu_s is the coefficient of static friction between the tyres and the wall. Substituting both results,

    mg≤μsmv2rmg \le \mu_s \dfrac{mv^{2}}{r}

    The mass cancels — the answer does not depend on how heavy the machine is:

    v2≥rgμsv^{2} \ge \dfrac{rg}{\mu_s}

    Result

     vmin⁡=rgμs \boxed{\,v_{\min} = \sqrt{\dfrac{rg}{\mu_s}}\,}

    Below this speed the wall cannot press hard enough for friction to carry the weight and the rider slides down. Note what the expression does **not** contain: the mass of the rider and machine, so a heavier rider needs exactly the same minimum speed.

  7. 7
    Moment of inertia of a uniform disc about a perpendicular axis through its centre
    Obtain an expression for the moment of inertia of a uniform disc of mass 'M' and radius 'R' rotating about an axis passing through its centre and perpendicular to its plane.

    Asked in: June 2025 (Q.3, 2 marks)

    Show the derivation
    Expression of M.I of uniform disc about an axis passing through its centre and perpendicular to its plane:
    Step 1
    Let, M = mass of disc, R = radius of disc, ZZ' = axis passing through the centre of disc and perpendicular to the plane.
    Step 2
    The M.I of a thin uniform disc about an axis passing through its centre and perpendicular to its plane is given by,
    IC=12MR2I_C=\dfrac{1}{2}MR^2
  8. 8
    Torque on a rigid body rotating with constant angular acceleration Repeats
    Obtain an expression for torque acting on a rigid body rotating with constant angular acceleration.

    Asked in: July 2016; June 2025 (Q.15, 3 marks)

    Show the derivation
    Step 1
    Consider a rigid object rotating with a constant angular acceleration 'α' about an axis perpendicular to the plane of paper.
    Step 2
    Let us consider the object to be consisting of N number of particles of masses m1,m2,....mNm_1,m_2,....m_N at respective perpendicular distances r1,r2,....rNr_1,r_2,....r_N from the axis of rotation.
    Step 3
    As the object rotates, all these particles perform circular motion with same angular acceleration α, but with different linear (tangential) accelerations a1=r1α,a2=r2α,....,aN=rNαa_1=r_1\alpha, a_2=r_2\alpha,....,a_N=r_N\alpha,etc.
    Step 4
    Force experienced by the first particle is, f1=m1a1=m1r1αf_1=m_1a_1=m_1r_1\alpha
    Step 5
    As these forces are tangential, the irrespective perpendicular distances from the axis are r1,r2,.....rNr_1,r_2,.....r_N.
    Step 6
    Thus, the torque experienced by the first particle is of magnitude τ1=f1r1=m1r12α\tau_1=f_1r_1=m_1r_1^2\alpha
    Similarly, τ2=m2r22α,τ3=m3r32α....τN=mNrN2α\tau_2=m_2r_2^2\alpha, \tau_3=m_3r_3^2\alpha....\tau_N=m_Nr_N^2\alpha
    Step 7
    If the rotation is restricted to a single plane, directions of all these torques are the same, and along the axis.
    Step 8
    Magnitude of the resultant torque is then given by
    τ=τ1+τ2+....+τN\tau=\tau_1+\tau_2+....+\tau_N
    =(m1r12+m2r22....+mNrN2)α=Iα=(m_1r_1^2+m_2r_2^2....+m_Nr_N^2)\alpha=I\alpha
    where, I=m1r12+m2r22....+mNrN2I=m_1r_1^2+m_2r_2^2....+m_Nr_N^2 is the moment of inertia of the object about the given axis of rotation.
    ii. Illustration: Ballet dancers: a. During ice ballet, the dancers have to undertake rounds of smaller and larger radii. b. The dancers come together by taking rounds of smaller radius (near the centre). c. In this case, the moment of inertia of their system becomes minimum and the frequency increases, to make it thrilling. d. While during outer rounds, the dancers outstretch their legs and arms. e. This increases their moment of inertia that reduces the angular speed and hence the linear speed. This is essential to prevent slipping.
  9. 9
    Maximum safety speed on a curved horizontal road (banking of roads)
    Obtain an expression for the maximum safety speed with which a vehicle should move along a curved horizontal road.

    Asked in: February 2026 (Q.28, 4 marks)

    Show the derivation
    Step 1
    The vertical section of a vehicle on a curved road of radius 'r' banked at an angle 'θ' with the horizontal is shown in the figure.
    Step 2
    Considering the vehicle to be a point and ignoring friction (not eliminating) and other non-conservative forces like air resistance, there are two forces acting on the vehicle: a. weight (mg), vertically downwards; b. normal reaction (N), perpendicular to the surface of the road.
    Step 3
    As the motion of the vehicle is along a horizontal circle, the resultant force must be horizontal and directed towards the centre of the track. Hence, the vertical force mg must be balanced.
    Step 4
    Thus, normal reaction (N) is resolved into: a. Nsinθ - along the horizontal. b. Ncosθ - along the vertical.
    Step 5
    The vertical component Ncosθ balances the weight,
    ∴Ncos⁡θ=mg\therefore N\cos\theta = mg ....(1)
    Step 6
    Horizontal component Nsinθ being the resultant force, must be the necessary centripetal force (or balance the centrifugal force).
    ∴Nsin⁡θ=mv2r\therefore N\sin\theta = \dfrac{mv^2}{r} ....(2)
    Dividing equation (2) by equation (1),
    tan⁡θ=v2rg\tan\theta = \dfrac{v^2}{rg}
    Step 7
    Thus, most safe speed, vs=rgtan⁡θv_s = \sqrt{rg\tan\theta}
    Step 8
    As the equation doesnot contain mass m, it is independent of mass of the vehicle.
  10. 10
    Period of a conical pendulum
    Derive an expression for the period of a conical pendulum.

    Asked in: March 2008

    Show the derivation
    Step 1
    Consider the vertical section of a conical pendulum having bob (point mass) of mass m and string of length 'L'.
    Step 2
    Here, θ is the angle made by the string with the vertical, at any position (semi-vertical angle of the cone).
    Step 3
    In a given position B, the forces acting on the bob are: a. its weight 'mg' directed vertically downwards; b. the force 'T₀' due to the tension in the string, directed along the string, towards the support A.
    Step 4
    As the motion of the bob is a horizontal circular motion, the resultant force must be horizontal and directed towards the centre C of the circular motion.
    Step 5
    For this, tension (T₀) in the string is resolved into: a. T₀cosθ : vertical component; b. T₀sinθ : horizontal component
    Step 6
    The vertical component (T₀cosθ) balances the weight 'mg'.
    ∴mg=T0cos⁡θ\therefore mg = T_0\cos\theta ....(1)
    Step 7
    The horizontal component T₀sinθ then becomes the resultant force which is centripetal.
    mrω2=T0sin⁡θmr\omega^2 = T_0\sin\theta ....(2)
    Dividing equation (2) by equation (1),
    ω2=gsin⁡θrcos⁡θ....(3)\omega^2 = \dfrac{g\sin\theta}{r\cos\theta}\qquad....(3)
    Step 8
    From the figure, sin⁡θ=rL\sin\theta = \dfrac{r}{L}
    ∴r=Lsin⁡θ\therefore r = L\sin\theta ....(4)
    From equation (3) and (4),
    ω2=gsin⁡θLsin⁡θcos⁡θ\omega^2 = \dfrac{g\sin\theta}{L\sin\theta\cos\theta}
    ω=gLcos⁡θ\omega = \sqrt{\dfrac{g}{L\cos\theta}}
    Step 9
    If T is the period of revolution of the bob, then
    ω=2πT=gLcos⁡θ\omega = \dfrac{2\pi}{T} = \sqrt{\dfrac{g}{L\cos\theta}}
    ∴\therefore Period, T=2πLcos⁡θgT = 2\pi\sqrt{\dfrac{L\cos\theta}{g}}
  11. 11
    Conical pendulum: relation tan⁡θ=v2/rg\tan\theta = v^2/rg
    For a conical pendulum, prove that tan⁡θ=v2rg\tan\theta = \dfrac{v^2}{rg}.

    Asked in: October 2009

    Show the derivation
    Step 1
    Consider a bob of mass m tied to one end of a string of length 'l' and other end is fixed to rigid support.
    Step 2
    Let the bob be displaced from its mean position and whirled around a horizontal circle of radius 'r' with constant angular velocity ω, then the bob performs U.C.M.
    Step 3
    During the motion, string is inclined to the vertical at an angle θ as shown in the figure.
    S : rigid support; T : tension in the string; l : length of string; h : height of support from bob; v : velocity of bob; r : radius of horizontal circle; θ : semi vertical angle; mg : weight of bob
    Step 4
    In the displaced position P, there are two forces acting on the bob: a. The weight mg acting vertically downwards. b. The tension T acting upward along the string.
    Step 5
    The tension (T) acting in the string can be resolved into two components: a. Tcosθ acting vertically upwards. b. Tsinθ acting horizontally towards centre of the circle.
    Step 6
    Vertical component Tcosθ balances the weight and horizontal component Tsinθ provides the necessary centripetal force.
    ∴Tcos⁡θ=mg\therefore T\cos\theta = mg ....(1)
    Tsin⁡θ=mv2r=mrω2T\sin\theta = \dfrac{mv^2}{r} = mr\omega^2 ....(2)
    Step 7
    Dividing equation (2) by (1), we get
    tan⁡θ=v2rg\tan\theta = \dfrac{v^2}{rg}
  12. 12
    Vertical circular motion: difference in tensions at the highest and lowest points
    A particle of mass m just completes vertical circular motion. Derive the expression for the difference in tensions at the highest and the lowest points.

    Asked in: March 2013

    Show the derivation
    Step 1
    Consider a particle of mass m moving along a vertical circle.
    Step 2
    At any position of the particle, there are only two forces acting on the particle: a. weight (mg), vertically downwards, which is constant; b. the force due to the tension (T), directed towards the centre. (Its magnitude changes periodically with time and location.)
    Step 3
    As the motion is non uniform, the resultant of these two forces is not directed towards the centre except at the uppermost and the lowermost positions of the bob.
    Step 4
    Uppermost position (A): a. Both, weight (mg) and force due to tension (TAT_A) are downwards, i.e., towards the centre. In this case, their resultant is used only as the centripetal force. b. Thus, if vAv_A is the speed at the uppermost point,
    mg+TA=mvA2r....(1)mg + T_A = \dfrac{mv_A^2}{r}\qquad....(1)
    c. For minimum possible speed at this point (or if the motion is to be realized with minimum possible energy), TA=0T_A = 0
    ∴(vA)min=rg....(2)\therefore (v_A)_{min} = \sqrt{rg}\qquad....(2)
    Step 5
    Lowermost position (B): a. Force due to the tension, TBT_B is vertically upwards, i.e., towards the centre, and opposite to mg. In this case, their resultant is the centripetal force. b. If vBv_B is the speed at the lowermost point,
    TB−mg=mvB2r....(3)T_B - mg = \dfrac{mv_B^2}{r}\qquad....(3)
    c. While coming down from the uppermost to the lowermost point, the vertical displacement is 2r and the motion is governed only by gravity. d. Hence the corresponding decrease in the gravitational potential energy is converted into the kinetic energy.
    ∴mg(2r)=12mvB2−12mvA2\therefore mg(2r) = \dfrac{1}{2}mv_B^2-\dfrac{1}{2}mv_A^2
    ∴vB2−vA2=4rg....(4)\therefore v_B^2-v_A^2 = 4rg\qquad....(4)
    Step 6
    Difference between the extreme tensions: Subtracting equation (1) from equation (3),
    TB−TA−2mg=mr(vB2−vA2)....(5)T_B-T_A-2mg = \dfrac{m}{r}(v_B^2-v_A^2)\qquad....(5)
    Using equation (4) and rearranging, we get,
    ∴TB−TA=6mg\therefore T_B-T_A = 6mg
    Hence, difference in tension at extreme positions depends only on weight.
  13. 13
    Theorem of perpendicular axes
    State and prove the theorem of perpendicular axes.

    Asked in: March 2010

    Show the derivation
    StatementThe moment of inertia of a laminar object about an axis (Z) perpendicular to its plane is the sum of its moment of inertia about two mutually perpendicular axes (X and Y) in its plane, all the three axes being concurrent.
    Mathematically, Iz=Ix+IyI_z = I_x+I_y
    Proof
    Step 1
    Consider a rigid laminar object able to rotate about three mutually perpendicular axes X, Y and Z.
    Step 2
    Axes X and Y are in the plane of the object while the Z axis is perpendicular to it, and all are concurrent at O.
    Step 3
    Consider a mass element dm located at any point P. PM = y and PN = x are the perpendiculars drawn from P respectively on the X and Y axes.
    Step 4
    The respective perpendicular distances of point P from X, Y and Z axes will then be y, x and y2+x2\sqrt{y^2+x^2}.
    Step 5
    If IxI_x, IyI_y and IzI_z are the respective moment of inertia of the body about x, y and z axes, then
    Ix=∫y2dm,Iy=∫x2dm,Iz=∫(y2+x2)dmI_x=\int y^2dm,\quad I_y=\int x^2dm,\quad I_z=\int(y^2+x^2)dm
    ∴Iz=∫y2dm+∫x2dm=Ix+Iy\therefore I_z=\int y^2dm+\int x^2dm=I_x+I_y
    This is the mathematical form of the theorem of perpendicular axes.
  14. 14
    Kinetic energy of a rolling body (translation + rotation)
    Derive an expression for kinetic energy when a rigid body is rolling on a horizontal surface without slipping. Hence find the kinetic energy for a solid sphere.

    Asked in: March 2013

    Show the derivation
    Expression for kinetic energy of rolling sphere:
    Step 1
    Mass of the sphere is given to be M. Let, v = linear velocity of the sphere, ω = angular velocity of the sphere, I = moment of inertia of the sphere, K = radius of gyration
    Step 2
    Total K.E of rolling body =(K.E)translational+(K.E)rotational=(K.E)_{translational}+(K.E)_{rotational}
    ∴(K.E)rolling=12Mv2+12Iω2=12Mv2+12MK2[v2r2](∵I=MK2 and v=rω)\therefore (K.E)_{rolling}=\dfrac{1}{2}Mv^2+\dfrac{1}{2}I\omega^2=\dfrac{1}{2}Mv^2+\dfrac{1}{2}MK^2\left[\dfrac{v^2}{r^2}\right]\qquad(\because I=MK^2\text{ and }v=r\omega)
    ∴(K.E)rolling=12Mv2[1+K2r2]....(1)\therefore (K.E)_{rolling}=\dfrac{1}{2}Mv^2\left[1+\dfrac{K^2}{r^2}\right]\qquad....(1)
    Since the value of 'K' is different for different bodies, so (K.E)rolling(K.E)_{rolling} also varies from body to body.

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