Statics and Dynamics Quiz: Mass Moment Of Inertia

13 questions · exam conditions

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Mass Moment Of InertiaQuestion 1 of 13

A rigid body rotates freely (no external torques) about a fixed axis. A small piece of mass $\Delta m$ suddenly detaches from the body at the instant it passes through the rotation axis (i.e., at zero radius from the axis). Which of the following best describes the effect on the body's angular velocity $\omega$ immediately after the mass detaches?

\omega

increases, because the total moment of inertia decreases when mass is lost, and angular momentum conservation requires a compensating increase in angular velocity.

\omega

remains unchanged, because the detached piece was located at the rotation axis and therefore contributed zero moment of inertia to the system; the angular momentum and moment of inertia of the remaining body are unaffected.

\omega

decreases, because the detached piece carries away a portion of the system's angular momentum proportional to its mass, leaving the remaining body with reduced angular momentum and therefore reduced angular velocity.

\omega

remains unchanged only if the detached piece leaves with zero velocity; if it leaves with any velocity, angular momentum is not conserved and

\omega

changes by an amount that depends on the direction of ejection.

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Statics and Dynamics Quiz

Statics and Dynamics Quiz: Mass Moment Of Inertia

Practice Mass Moment Of Inertia in Statics and Dynamics with focused quiz questions that help you check what you know, review explanations, and build confidence with test-style prompts.

What this quiz covers

This quiz focuses on Mass Moment Of Inertia, giving you a quick way to practice the rules, question types, and explanations that matter most for Statics and Dynamics.

How to use this quiz

Try each quiz question before looking at the correct answer. Use the explanations to review missed ideas, then come back to similar questions until the pattern feels familiar.

All questions

Question 1

$\omega$ increases, because the total moment of inertia decreases when mass is lost, and angular momentum conservation requires a compensating increase in angular velocity.
$\omega$ remains unchanged, because the detached piece was located at the rotation axis and therefore contributed zero moment of inertia to the system; the angular momentum and moment of inertia of the remaining body are unaffected. (correct answer)
$\omega$ decreases, because the detached piece carries away a portion of the system's angular momentum proportional to its mass, leaving the remaining body with reduced angular momentum and therefore reduced angular velocity.
$\omega$ remains unchanged only if the detached piece leaves with zero velocity; if it leaves with any velocity, angular momentum is not conserved and $\omega$ changes by an amount that depends on the direction of ejection.

Explanation: Whenever you see a rigid-body rotation problem involving a detaching piece, your first instinct should be to apply conservation of angular momentum — but carefully. The key equation is

L = I\omega

, where the moment of inertia

I = \sum m_i r_i^2

depends critically on each particle's distance

r_i

from the rotation axis. Here, the piece

\Delta m

detaches precisely when it passes through the rotation axis, meaning its radial distance is

r = 0

at that instant. This means it contributed exactly

\Delta m \cdot (0)^2 = 0

to the total moment of inertia before detachment. When it leaves, the system's moment of inertia doesn't change at all. Furthermore, a mass sitting at

r = 0

has zero tangential velocity (since

v = r\omega = 0

), so it carries away zero angular momentum. The remaining body therefore retains the same

L

and the same

I

, leaving

\omega

completely unchanged. B is correct. Choice A applies the right logic (

I

decreases →

\omega

increases) to the wrong situation — that reasoning only holds when mass is removed at a nonzero radius, where it genuinely reduces

I

. Choice C assumes the detached piece carries away angular momentum proportional to its mass, ignoring that angular momentum depends on

mvr

, not mass alone. At

r = 0

, that contribution is zero regardless of

\Delta m

. Choice D introduces an unnecessary complication. The ejection velocity is irrelevant here because no matter what direction

\Delta m

leaves, it had zero angular momentum about the axis at the moment of detachment. Study tip: Always evaluate a detaching mass's contribution using

\Delta I = \Delta m \cdot r^2

. If

r = 0

, the mass is dynamically invisible to the rotation — it changes nothing.

Question 2

A turntable (moment of inertia $I_T$ ) spins freely at $\omega_0$ . A student standing at the center of the turntable (moment of inertia $I_S$ about the vertical axis) holds a spinning bicycle wheel (moment of inertia $I_W$ about its axle) with its spin axis vertical, rotating at angular speed $\Omega$ relative to the student in the same direction as the turntable. The student flips the wheel so its axle remains vertical but its spin direction relative to the student is reversed. Which expression correctly gives the final angular velocity $\omega_f$ of the turntable–student system after the flip?

$\omega_f = \dfrac{(I_T + I_S)\omega_0 + 2I_W\Omega}{I_T + I_S}$ , which neglects the wheel's contribution to the final moment of inertia by treating it as mechanically decoupled from the platform after the flip.
$\omega_f = \dfrac{(I_T + I_S + I_W)\omega_0 + 2I_W\Omega}{I_T + I_S + I_W}$ , derived by correctly accounting for the wheel's absolute angular momentum before and after the flip using the rolling platform as the reference. (correct answer)
$\omega_f = \dfrac{(I_T + I_S)\omega_0 + I_W(\omega_0 + \Omega)}{I_T + I_S + I_W}$ , which misassigns the wheel's initial angular momentum as $I_W(\omega_0+\Omega)$ but does not consistently track the change upon reversal.
$\omega_f = \dfrac{(I_T + I_S + I_W)\omega_0 + 2I_W\Omega}{I_T + I_S}$ , which inflates the numerator with the full initial angular momentum but incorrectly omits $I_W$ from the denominator in the final state.

Explanation: Whenever you see a problem involving a spinning system where an internal mechanism changes, your instinct should be conservation of angular momentum — but you must apply it carefully using absolute (lab-frame) angular momenta, not relative ones. Here's the key setup: the total angular momentum of the system (turntable + student + wheel) is conserved because no external torques act. Initially, the turntable–student system spins at

\omega_0

, and the wheel spins at

\Omega

relative to the student — but in the same direction as the platform. The wheel's absolute angular velocity is therefore

\omega_0 + \Omega

, giving an initial total angular momentum of:

L_i = (I_T + I_S)\omega_0 + I_W(\omega_0 + \Omega)

After the flip, the wheel's spin relative to the student reverses, so its absolute angular velocity becomes

\omega_f - \Omega

. Since the wheel is physically held by the student, the entire system rotates at

\omega_f

, meaning the final angular momentum is:

L_f = (I_T + I_S)\omega_f + I_W(\omega_f - \Omega)= (I_T + I_S + I_W)\omega_f - I_W\Omega

Setting

L_i = L_f

and solving gives exactly answer B:

\omega_f = \dfrac{(I_T + I_S + I_W)\omega_0 + 2I_W\Omega}{I_T + I_S + I_W}

. A is wrong because it drops

I_W

from the denominator, treating the wheel as disconnected from the platform after the flip — but the student is still holding it. C incorrectly assigns the initial wheel momentum as

I_W(\omega_0 + \Omega)

without properly tracking the reversal's effect on the final state. D inflates the numerator correctly but then erroneously omits

I_W

from the final moment of inertia in the denominator. Your study tip: always convert relative angular velocities to absolute (lab-frame) values before applying conservation of angular momentum — mixing frames is the most common trap in rotating-system problems.

Question 3

Two identical uniform disks, each of mass $m$ and radius $R$ , are initially spinning independently about their own central axes with angular velocities $+\omega_0$ and $-\omega_0$ (opposite directions). They are then brought into contact along their rims so that friction between the contact surfaces couples them. Assume the disks' axles remain fixed and parallel throughout.

After the disks reach a common steady-state condition, which of the following correctly describes the final state and the underlying moment-of-inertia reasoning?

Both disks spin at $\omega_0/2$ in opposite directions, because friction transfers angular momentum symmetrically between the disks, halving each disk's spin while preserving each individual disk's angular momentum separately.
Both disks continue spinning at $\omega_0$ in opposite directions indefinitely, because the rim velocities at the contact point are already matched — each rim moves at speed $R\omega_0$ in the same direction — so no friction force develops and neither disk decelerates.
Both disks come to rest, because the contact friction exerts decelerating torques on each disk simultaneously; with equal moments of inertia and equal torque magnitudes, the disks decelerate symmetrically, and the only state satisfying both zero total angular momentum and the no-slip rim condition is $\omega = 0$ for each disk. (correct answer)
The disk initially spinning at $+\omega_0$ continues at $+\omega_0$ while the disk at $-\omega_0$ reverses to $+\omega_0$ , because friction always acts to align spinning bodies into a common rotation direction, and total angular momentum is not conserved since the fixed axles exert external reaction forces.

Explanation: When two coupled rotating bodies share a contact point, you need to think about two constraints simultaneously: the no-slip condition at the rim (rim velocities must match at steady state) and conservation of angular momentum for the system — but only if no external torques act. Here, the fixed axles do exert external reaction forces, so angular momentum of the disks alone need not be conserved. That frees you to focus purely on the geometric and dynamic constraints. At the moment of contact, disk 1 has rim velocity

+R\omega_0

and disk 2 has rim velocity

-R\omega_0

— they point in opposite directions at the contact point, creating a large relative slip and therefore strong friction. Friction decelerates disk 1 (negative torque) and accelerates disk 2 toward less negative spin (positive torque). Because the disks are identical (same

I = \frac{1}{2}mR^2

) and experience equal-magnitude torques, they decelerate symmetrically. The no-slip condition requires the final rim speeds to match:

R\omega_f = R\omega_f

, which for equal-and-opposite initial conditions gives

\omega_f = 0

. Both disks stop. C is correct. Choice A is wrong because it misapplies a "momentum-sharing" shortcut — angular momentum isn't conserved here due to axle reactions, and

\omega_0/2

satisfies neither the no-slip condition nor the torque symmetry. Choice B is wrong because the rim velocities are opposite in direction at the contact point (

+R\omega_0

vs.

-R\omega_0

), not matched — there is absolutely a velocity difference driving friction. Choice D is wrong because friction doesn't "align" spins; it enforces the no-slip condition, which here demands rest. Your study tip: always check direction of rim velocities at the contact point, not just magnitude. That one step prevents both the B and D traps.

Question 4

Hoop and disk: same mass, radius. Ratio of radii of gyration k_hoop/k_disk?

√2 times (correct answer)
2 times
1/2 times
1 time

Explanation: Radius of gyration is sqrt(I/m). For a hoop, I = mR^2, so k_hoop = R. For a solid disk, I = (1/2)mR^2, so k_disk = R/sqrt(2). Dividing gives sqrt(2). The tempting mistake is comparing moments of inertia directly and saying 2 times, without taking the square root to get k.

Question 5

Identical rods: one pivoted at center, one at end. Same angular acceleration needed. Which requires more torque?

End pivot, 4 times torque (correct answer)
Center pivot, 4 times torque
Both need the same torque
Center pivot, same torque

Explanation: Torque equals moment of inertia times angular acceleration. The end pivot has I = mL^2/3, while the center pivot has I = mL^2/12, a four-times-larger moment of inertia. With the same angular acceleration, the end pivot needs four times the torque. The tempting mistake is thinking both need the same torque, but the rod's mass is distributed farther from the end pivot, raising its rotational inertia.

Question 6

Two flywheels have equal angular momentum. A has the larger moment of inertia. Which statement is true?

A has the larger angular speed
A has greater kinetic energy
Both have equal kinetic energy
A has smaller kinetic energy (correct answer)

Explanation: Angular momentum is I times angular speed, and kinetic energy is L squared divided by 2I. With equal angular momentum, the flywheel with the larger moment of inertia has the smaller kinetic energy. The tempting mistake is thinking larger inertia means more energy, but for fixed angular momentum energy actually decreases as inertia increases.

Question 7

Same dumbbell, same angular speed, spun about its center vs one end. Center rotational KE is what multiple of end?

Twice as much
Same amount
Half as much (correct answer)
Four times

Explanation: For a dumbbell of two equal masses distance L apart, moment of inertia about the center is 2m(L/2)^2 = mL^2/2; about one end it is m(0)^2 + mL^2 = mL^2. Since rotational KE = (1/2)Iω^2 and ω is the same, the center KE is half. The tempting wrong choice is 'same amount': same angular speed doesn't mean same KE because the end axis puts one mass farther from the axis, doubling I.

Question 8

A uniform thin rod of mass $m$ and length $L$ is welded perpendicularly to the rim of a uniform disk of mass $M$ and radius $R$ , with the rod extending radially outward from the rim. The assembly rotates about the disk's central axis (perpendicular to the disk and through its center). Which expression correctly gives the total moment of inertia of the assembly about the disk's central axis?

$I = \frac{1}{2}MR^2 + \frac{1}{3}mL^2 + mR^2$ , using the parallel-axis theorem to shift the rod's centroidal moment of inertia ( $\frac{1}{12}mL^2$ ) to the rod's near end, then treating the near end as being at radius $R$ from the disk's axis.
$I = \frac{1}{2}MR^2 + \frac{1}{3}mL^2$ , treating the rod as rotating about one of its ends which coincidentally sits at the disk's rim, so no additional parallel-axis shift is needed beyond the standard end-pivot formula.
$I = \frac{1}{2}MR^2 + m\left(R + \frac{L}{2}\right)^2$ , treating the rod as a point mass at its center of mass located at distance $R + L/2$ from the disk's central axis, which is exact for a slender rod rotating about an external axis.
$I = \frac{1}{2}MR^2 + \frac{1}{12}mL^2 + m\left(R + \frac{L}{2}\right)^2$ , applying the parallel-axis theorem by shifting the rod's centroidal moment of inertia $\frac{1}{12}mL^2$ by the distance from the rod's own center of mass to the disk's central axis. (correct answer)

Explanation: Whenever you encounter a composite rigid body rotating about an axis, your go-to tool is the parallel-axis theorem:

I = I_{cm} + md^2

, where

d

is the distance from the object's own center of mass to the rotation axis. Applied correctly to each component, you simply sum the results. For this assembly, the disk spins about its own central axis, so its contribution is straightforwardly

\frac{1}{2}MR^2

. The rod is trickier. Its center of mass sits at distance

R + \frac{L}{2}

from the disk's central axis —

R

to reach the rim, then another

\frac{L}{2}

to the rod's midpoint. Applying the parallel-axis theorem to the rod: take its centroidal moment of inertia

\frac{1}{12}mL^2

and shift it by

d = R + \frac{L}{2}

, giving

\frac{1}{12}mL^2 + m\!\left(R + \frac{L}{2}\right)^2

. The total is therefore

I = \frac{1}{2}MR^2 + \frac{1}{12}mL^2 + m\!\left(R + \frac{L}{2}\right)^2

, confirming D. Choice A misapplies the parallel-axis theorem by first shifting the rod's moment of inertia to its near end (producing

\frac{1}{3}mL^2

) and then adding

mR^2

as a second shift — you cannot apply the parallel-axis theorem twice in sequence like that. Choice B uses the end-pivot formula

\frac{1}{3}mL^2

as if the disk's axis passes through the rod's near end, which it does not — the axis is a distance

R

away. Choice C treats the rod as a point mass, ignoring its rotational inertia about its own center of mass; this omits the

\frac{1}{12}mL^2

term entirely. The key study tip: always apply the parallel-axis theorem once, shifting from the object's own centroid to the system's rotation axis. Never double-shift, and never approximate an extended body as a point mass unless the problem explicitly permits it.

Question 9

A uniform solid cylinder and a thin-walled hollow cylinder have identical mass $m$ and identical outer radius $R$ . Both are released from rest at the top of an identical inclined plane and roll without slipping to the bottom.

Which of the following correctly explains why the solid cylinder reaches the bottom first, and what this reveals about the relationship between mass moment of inertia and rotational dynamics?

The solid cylinder has a smaller mass moment of inertia ( $I = \frac{1}{2}mR^2$ ) than the hollow cylinder ( $I = mR^2$ ), so for the same gravitational torque input, the solid cylinder develops greater angular acceleration and converts a larger fraction of potential energy into translational kinetic energy rather than rotational kinetic energy. (correct answer)
The solid cylinder has a smaller mass moment of inertia, so it stores more rotational kinetic energy for the same angular velocity, which means friction does more negative work on it and reduces its translational speed less than for the hollow cylinder.
The hollow cylinder has a larger mass moment of inertia and therefore a larger radius of gyration, which increases the rolling constraint force and reduces the net tangential force available for translational acceleration, but the total mechanical energy at the bottom is the same for both cylinders.
Both cylinders experience the same gravitational potential energy loss, but the solid cylinder's lower moment of inertia means it requires less torque to maintain rolling, so the friction force at the contact point is smaller and the translational acceleration is larger by the same factor as the inertia ratio.

Explanation: When a cylinder rolls without slipping down an incline, its gravitational potential energy splits between translational kinetic energy (

\frac{1}{2}mv^2

) and rotational kinetic energy (

\frac{1}{2}I\omega^2

). The rolling constraint ties these together:

v = R\omega

. A larger moment of inertia means more energy goes into rotation, leaving less for translation — and slower linear speed at the bottom. Choice A captures this correctly. The solid cylinder's moment of inertia is

I = \frac{1}{2}mR^2

, while the hollow cylinder's is

I = mR^2

. Setting

mgh = \frac{1}{2}mv^2 + \frac{1}{2}I\omega^2

and substituting

\omega = v/R

, you can show the solid cylinder reaches a higher translational speed at the bottom and therefore arrives first. Its lower inertia also means greater angular acceleration for the same net torque, reinforcing the same conclusion from a dynamics perspective. A is correct. Choice B is wrong in a critical way: a smaller moment of inertia stores less rotational energy at a given

\omega

, not more. The logic is inverted. Choice C correctly identifies that total mechanical energy is conserved for both, but mischaracterizes the friction force as directly reducing net translational force in a way that harms the solid cylinder — friction here is a constraint force enabling rolling, not pure negative work. Choice D is wrong because it claims the solid cylinder needs less torque to "maintain rolling," a vague and misleading idea; the real mechanism is energy partitioning, not torque maintenance. Your takeaway: whenever rolling problems appear, immediately write the energy equation with both kinetic terms and substitute

\omega = v/R

. The moment of inertia ratio directly tells you which object translates faster.

Question 10

A rigid, non-uniform body has its center of mass at point G. An engineer measures the moment of inertia about an axis through G and obtains $I_G$ . She then measures the moment of inertia about a parallel axis through point P, located a distance $d$ from G, and obtains $I_P$ . A colleague proposes measuring the moment of inertia about a third parallel axis through point Q, which is located a distance $d$ from P (not from G) along the same direction. Which expression correctly gives $I_Q$ ?

$I_Q = I_G + m(2d)^2$ , because Q is at distance $2d$ from G (since P is at distance $d$ from G and Q is at distance $d$ from P in the same direction), and the parallel-axis theorem applies directly from the center-of-mass axis. (correct answer)
$I_Q = I_P + md^2$ , because the parallel-axis theorem allows transfer between any two parallel axes by adding $md^2$ where $d$ is the distance between those two axes, regardless of whether either axis passes through the center of mass.
$I_Q = I_G + m(d + \sqrt{I_P - I_G)/m})^2$ , because the distance from G to Q must be computed using the intermediate distance from G to P derived from $I_P$ , then extended by $d$ to reach Q.
$I_Q = I_G + m(2d)^2$ only if P lies between G and Q; if Q is on the opposite side of P from G, then $I_Q = I_G + m \cdot 0 = I_G$ , because the displacements cancel and Q coincides with G.

Explanation: Whenever you see a question involving the parallel-axis theorem, your first instinct should be: every application of this theorem must anchor back to the center-of-mass axis. The theorem states

I = I_G + mr^2

, where

r

is the distance from the center of mass G to the new axis — not the distance between any two arbitrary axes. Since P is distance

d

from G, and Q is distance

d

from P in the same direction, Q lies at distance

2d

from G. Applying the parallel-axis theorem correctly from G gives

I_Q = I_G + m(2d)^2

, which is answer A. This is always valid because G is the reference anchor for the theorem. Answer B is the most tempting trap. It claims you can "chain" the parallel-axis theorem — transferring from P to Q by simply adding

md^2

. This is wrong because the parallel-axis theorem only works when one of the axes passes through the center of mass. You cannot hop from one arbitrary axis to another; doing so accumulates error and has no physical justification. Answer C introduces unnecessary algebra. Since the problem explicitly states P is distance

d

from G, you don't need to back-calculate that distance from

I_P

. The geometry is already given. Answer D contains a fundamental geometry error. If G is at position 0, P is at

d

, and Q is at

2d

in the same direction, Q never coincides with G — displacements don't "cancel" here. Q is at

2d

from G regardless of ordering. Study tip: Always ask "what is the distance from G?" before applying the parallel-axis theorem. If G isn't one of your two axes, you must first return to G, then transfer outward.

Question 11

Two flywheels, A and B, have equal mass $m$ and are both rotating at the same angular velocity $\omega_0$ . Flywheel A is a uniform solid disk of radius $R$ ; flywheel B is an annular disk (ring) with inner radius $R/2$ and outer radius $R$ . A braking torque of identical magnitude $\tau$ is applied to each flywheel. Which flywheel takes longer to stop, and by approximately what factor?

Flywheel B takes longer to stop by a factor of $\frac{5}{4}$ , because its moment of inertia $I_B = \frac{5}{8}mR^2$ exceeds $I_A = \frac{1}{2}mR^2$ , and stopping time is proportional to $I$ for a given $\tau$ and $\omega_0$ . (correct answer)
Flywheel B takes longer to stop by a factor of $\frac{3}{2}$ , because removing material from the center of flywheel B reduces its mass near the axis, causing a disproportionate increase in the effective braking radius and reducing the required angular deceleration.
Flywheel A takes longer to stop by a factor of $\frac{4}{5}$ , because a solid disk distributes mass all the way to the center, giving it greater rotational inertia per unit mass at inner radii compared with the hollow annulus.
Both flywheels take exactly the same time to stop, because they have equal mass and equal outer radius $R$ ; since the applied braking torque acts at the outer rim, the angular deceleration is identical for both regardless of internal mass distribution.

Explanation: Whenever a question asks about rotational stopping time, your instinct should be to reach for Newton's second law for rotation:

\alpha = \tau / I

. Since stopping time is

t = \omega_0 / \alpha = I\omega_0 / \tau

, the flywheel with greater moment of inertia takes longer to stop — full stop. Start by computing each moment of inertia. For a solid disk,

I_A = \frac{1}{2}mR^2

. For an annular disk with inner radius

r_1 = R/2

and outer radius

r_2 = R

, the formula is

I = \frac{1}{2}m(r_1^2 + r_2^2)

, giving

I_B = \frac{1}{2}m\!\left(\frac{R^2}{4} + R^2\right) = \frac{1}{2}m \cdot \frac{5R^2}{4} = \frac{5}{8}mR^2

. Since

I_B > I_A

, flywheel B decelerates more slowly and takes longer to stop. The ratio of stopping times is

t_B / t_A = I_B / I_A = \frac{5/8}{1/2} = \frac{5}{4}

. That confirms A is correct. Choice B arrives at the right conclusion (B stops later) but invents a false physical explanation about "effective braking radius" — the torque magnitude is given as identical, so no such effect applies. Choice C gets the comparison backwards: the annulus, not the solid disk, has the larger moment of inertia, because its mass is concentrated farther from the axis. Choice D is a classic trap — equal mass and equal outer radius do not guarantee equal moment of inertia. Internal mass distribution matters enormously. Your study tip: memorize that

I_{\text{annulus}} = \frac{1}{2}m(r_1^2 + r_2^2)

and always ask where the mass sits relative to the axis, not just how much mass there is.

Question 12

An engineer is designing a system where a uniform solid sphere (mass $m$ , radius $r$ ) rolls without slipping inside a fixed hollow spherical shell of radius $R$ (with $R \gg r$ ). The small sphere oscillates back and forth through the bottom of the shell like a pendulum. The engineer models this as a physical pendulum with effective length $\ell_{eff}$ .

Which expression correctly gives $\ell_{eff}$ for the small rolling sphere, and which moment of inertia concept is central to deriving it?

$\ell_{eff} = \frac{2}{5}(R - r)$ , derived because the sphere's moment of inertia $I_{cm} = \frac{2}{5}mr^2$ directly scales the effective pendulum length through the ratio $I_{cm}/(mr^2)$ applied to the geometric arc radius $R - r$ .
$\ell_{eff} = (R - r)$ , derived by treating the sphere's center of mass as executing circular motion of radius $R - r$ about the shell's center; since the sphere is small ( $r \ll R$ ), its rotational inertia about its own center is negligible and the system behaves as a simple pendulum.
$\ell_{eff} = \frac{5}{7}(R - r)$ , derived because the rolling constraint reduces the effective gravitational restoring force by the factor $\frac{5}{7}$ (the translational fraction of total energy for a rolling sphere), making the pendulum oscillate faster than a sliding sphere would.
$\ell_{eff} = \frac{7}{5}(R - r)$ , derived by accounting for the fact that rolling without slipping means the sphere's rotational kinetic energy (involving $I_{cm} = \frac{2}{5}mr^2$ ) augments the effective inertia, so the ratio $I_{total}/(mgd)$ yields an effective length larger than the geometric distance $R - r$ . (correct answer)

Explanation: Whenever you see a rolling-without-slipping problem framed as a pendulum, your instinct should be to treat it as a physical pendulum, where the period depends on total rotational inertia, not just the geometry. For a physical pendulum,

\omega^2 = \frac{mgd}{I_{pivot}}

, and the effective length is defined by

\ell_{eff} = \frac{I_{pivot}}{md}

, where

d = R - r

is the distance from the shell's center to the sphere's center of mass. The rolling constraint means the sphere both translates and rotates, so you must use the total moment of inertia about the pivot (shell center). By the parallel axis theorem:

I_{pivot} = I_{cm} + m(R-r)^2 = \frac{2}{5}mr^2 + m(R-r)^2

. Since

r \ll R

, the

\frac{2}{5}mr^2

term is negligible compared to

m(R-r)^2

... but wait — the rolling constraint links rotation about the sphere's own center to translation, effectively adding rotational inertia. Working through the Lagrangian or energy method properly gives

I_{eff} = \frac{7}{5}m(R-r)^2

, so

\ell_{eff} = \frac{I_{eff}}{m(R-r)} = \frac{7}{5}(R-r)

. This confirms D is correct: rolling augments the effective inertia by the familiar factor of

\frac{7}{5}

. Choice A incorrectly applies the ratio

I_{cm}/(mr^2)

directly to scale the geometric length — that's a fabricated shortcut with no physical basis. Choice B ignores rotational kinetic energy entirely, valid only for a sliding point mass. Choice C gets the fraction inverted:

\frac{5}{7}

describes the translational energy fraction, but applying it as a length reduction confuses energy partitioning with effective pendulum length. Your study tip: for any rolling-pendulum hybrid, always write the total kinetic energy (translational + rotational), then extract

\omega^2

by comparing to

\omega^2 = g/\ell_{eff}

. The factor

\frac{7}{5}

for a solid sphere appears repeatedly — memorize it.

Question 13

A spacecraft consists of a cylindrical main body (mass $M$ , radius $R$ , length $L$ , rotating about its symmetry axis) and two slender solar panel arms, each of mass $m$ and length $\ell$ , attached at the cylinder's surface and extending radially outward. The spacecraft spins freely with no external torques.

The solar panels are then retracted so they lie flush against the cylinder surface (effectively reducing each panel to a point mass at radius $R$ ). Ignoring the change in the cylinder's own inertia, which expression correctly gives the new angular velocity $\omega_f$ in terms of the initial angular velocity $\omega_i$ ?

$\omega_f = \omega_i \cdot \dfrac{\frac{1}{2}MR^2 + 2\left(\frac{1}{3}m\ell^2 + mR^2\right)}{\frac{1}{2}MR^2 + 2mR^2}$ , which would imply the spacecraft slows down when the panels retract.
$\omega_f = \omega_i \cdot \dfrac{\frac{1}{2}MR^2 + 2\left(m\ell^2 + mR^2\right)}{\frac{1}{2}MR^2 + 2mR^2}$ , treating each extended panel as a point mass concentrated at its far tip at distance $\ell + R$ from the axis.
$\omega_f = \omega_i \cdot \dfrac{\frac{1}{2}MR^2 + 2mR^2}{\frac{1}{2}MR^2 + 2\left(\frac{1}{3}m\ell^2 + mR^2\right)}$ , which correctly applies the parallel-axis theorem for a rod whose near end begins at radius $R$ from the spin axis. (correct answer)
$\omega_f = \omega_i \cdot \dfrac{\frac{1}{2}MR^2 + 2m\ell^2}{\frac{1}{2}MR^2 + 2mR^2}$ , omitting the offset term $mR^2$ from the initial panel inertia by assuming each panel pivots about the spacecraft's central axis directly.

Explanation: When a rotating system has no external torques, angular momentum is conserved:

L = I\omega = \text{constant}

. So

\omega_f = \omega_i \cdot \frac{I_i}{I_f}

. The key challenge here is correctly computing the initial moment of inertia of each extended solar panel. Each panel is a slender rod of mass

m

and length

\ell

, but its near end starts at radius

R

from the spin axis — it doesn't pivot from the center. To handle this, use the parallel-axis theorem: first find the rod's inertia about its own center (

\frac{1}{12}m\ell^2

), then shift to the spin axis, which is located

R + \frac{\ell}{2}

from the rod's center. That gives

\frac{1}{12}m\ell^2 + m\left(R + \frac{\ell}{2}\right)^2 = \frac{1}{3}m\ell^2 + mR\ell + mR^2

. Alternatively, you can integrate directly:

\int_R^{R+\ell} r^2\,\frac{m}{\ell}\,dr = \frac{1}{3}m\ell^2 + mR\ell + mR^2

. After retraction, each panel becomes a point mass at radius

R

, contributing

mR^2

. Choice C correctly reflects this physics, with

I_i > I_f

, so

\omega_f > \omega_i

— the spacecraft speeds up as mass moves inward. Choice A uses

\frac{1}{3}m\ell^2 + mR^2

, omitting the cross term

mR\ell

, which underestimates the initial inertia and reverses the speed-up conclusion. Choice B treats each panel as a point mass at its far tip (distance

\ell

from attachment), ignoring that the mass is distributed along the rod. Choice D drops the

mR^2

offset entirely, incorrectly assuming each rod pivots from the central axis rather than from radius

R

. Your study tip: whenever a rod doesn't start at the rotation axis, you must account for the offset — integrate from the true inner radius, or carefully apply the parallel-axis theorem. Forgetting the attachment offset is the most common trap on rotation problems like this.