Statics and Dynamics Quiz: Planar Rigid Body Motion
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Planar Rigid Body MotionQuestion 1 of 6

A uniform thin disk of mass mm and radius RR is attached at its center to a massless rod pinned at a fixed point O. The rod has length dd (measured from O to the disk center C). The disk is free to spin about the rod-disk pin at C (i.e., the disk can spin independently about the pin at C). The system swings in a vertical plane.

Compared to the same system but with the disk welded (fixed) to the rod so it cannot spin at C, how does the period of small oscillations change when the disk is free to spin at the pin?

The period increases when the disk is free to spin, because the effective moment of inertia about O is larger — the disk's spin degree of freedom adds kinetic energy storage without contributing to restoring torque, making the system dynamically 'heavier.'
The period decreases when the disk is free to spin, because the disk's rotational inertia about C does not contribute to the moment of inertia about O in the free-spin case (Idisk about O=md2I_{\text{disk about O}} = md^2 only, versus md2+12mR2md^2 + \frac{1}{2}mR^2 when welded), reducing the effective inertia and increasing the natural frequency.
The period remains the same regardless of whether the disk spins freely or is welded, because the restoring torque mgdsinϕmgd\sin\phi and the moment of inertia about O are both unchanged — the disk's spin at C is an internal degree of freedom that does not affect the pendulum's equation of motion.
The period remains the same only if dRd \gg R; otherwise the period increases when the disk is free to spin, because the gyroscopic effect of the freely spinning disk introduces a coupling between spin and swing that increases the effective inertia for small d/Rd/R ratios.
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Statics and Dynamics Quiz

Statics and Dynamics Quiz: Planar Rigid Body Motion

Practice Planar Rigid Body Motion 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 Planar Rigid Body Motion, giving you a quick way to practice the rules, question types, and explanations that matter most for Statics and Dynamics.

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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.

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Question 1

A uniform thin disk of mass mm and radius RR is attached at its center to a massless rod pinned at a fixed point O. The rod has length dd (measured from O to the disk center C). The disk is free to spin about the rod-disk pin at C (i.e., the disk can spin independently about the pin at C). The system swings in a vertical plane.

Compared to the same system but with the disk welded (fixed) to the rod so it cannot spin at C, how does the period of small oscillations change when the disk is free to spin at the pin?

  1. The period increases when the disk is free to spin, because the effective moment of inertia about O is larger — the disk's spin degree of freedom adds kinetic energy storage without contributing to restoring torque, making the system dynamically 'heavier.'
  2. The period decreases when the disk is free to spin, because the disk's rotational inertia about C does not contribute to the moment of inertia about O in the free-spin case (Idisk about O=md2I_{\text{disk about O}} = md^2 only, versus md2+12mR2md^2 + \frac{1}{2}mR^2 when welded), reducing the effective inertia and increasing the natural frequency. (correct answer)
  3. The period remains the same regardless of whether the disk spins freely or is welded, because the restoring torque mgdsinϕmgd\sin\phi and the moment of inertia about O are both unchanged — the disk's spin at C is an internal degree of freedom that does not affect the pendulum's equation of motion.
  4. The period remains the same only if dRd \gg R; otherwise the period increases when the disk is free to spin, because the gyroscopic effect of the freely spinning disk introduces a coupling between spin and swing that increases the effective inertia for small d/Rd/R ratios.
Explanation: When analyzing compound pendulums, your key tool is the rotational equation of motion: τ=IOϕ¨\tau = I_O \ddot{\phi}. The period depends on both the restoring torque and the effective moment of inertia about the pivot O, so you need to carefully identify what contributes to each. For the free-spin case, the disk can rotate independently at pin C. This means the disk's orientation in space is not coupled to the rod's angular displacement — the disk doesn't rotate with the rod. Consequently, the disk contributes only its translational (point-mass) inertia to the swing: IO=md2I_O = md^2. The restoring torque remains mgdsinϕmgdϕmgd\sin\phi \approx mgd\phi, giving a natural frequency ω=mgd/(md2)=g/d\omega = \sqrt{mgd/(md^2)} = \sqrt{g/d}. For the welded case, the disk is forced to rotate with the rod, so its spin inertia adds via the parallel axis theorem: IO=md2+12mR2I_O = md^2 + \frac{1}{2}mR^2. This larger inertia produces a lower frequency and longer period. Since the free-spin case has smaller effective inertia, its frequency is higher and its period is shorter — confirming B is correct. A is wrong because it claims the free-spin disk increases effective inertia. In reality, the disk's spin is unconstrained, so it contributes zero rotational inertia about O — not extra inertia. C is wrong because the moment of inertia about O does change between the two cases: welding adds 12mR2\frac{1}{2}mR^2, which is not negligible. D invents a gyroscopic coupling that doesn't exist in this planar, small-oscillation scenario. Study tip: When a component can spin freely at an internal pin, ask yourself — is its rotation forced by the system's coordinate? If not, it drops out of the effective inertia entirely.

Question 2

A rigid disk of radius RR and mass mm rolls without slipping on a flat horizontal surface. A horizontal force FF is applied at the center of the disk. A student claims: "Because the disk rolls without slipping, the friction force at the contact point does no work, so the work-energy theorem for the system gives Fs=12mvC2+12ICω2F \cdot s = \frac{1}{2}mv_C^2 + \frac{1}{2}I_C\omega^2, where ss is the displacement of the center." Which statement best evaluates this claim?

  1. The claim is incorrect: the work-energy equation must include the work done by the normal force from the ground, which acts over the vertical displacement of the contact point during deformation, so the equation should include a term NδN \cdot \delta for the ground's normal work.
  2. The claim is incorrect: the friction force does negative work on the disk equal to fs-f \cdot s (where ff is the friction force and ss is the displacement of the center), so the correct equation is (Ff)s=12mvC2+12ICω2(F - f) \cdot s = \frac{1}{2}mv_C^2 + \frac{1}{2}I_C\omega^2, and the claim understates the kinetic energy.
  3. The claim is correct in conclusion but flawed in reasoning: while the contact point does have zero instantaneous velocity, friction still does work in the rotational sense, so the correct justification is that the translational work of friction and its rotational work cancel exactly, leaving FsF \cdot s as the net work.
  4. The claim is correct: static friction at the contact point does no work because the contact point has zero velocity at every instant (it is the instantaneous center of rotation), so the work-energy equation as written is valid with FsF \cdot s as the only work input. (correct answer)
Explanation: Whenever you encounter rolling-without-slipping problems, the key question is: does friction do work? The answer hinges on where friction acts and what velocity that point has. For a disk rolling without slipping, the contact point is the instantaneous center of rotation — its velocity is exactly zero at every instant. Since work is defined as dW=FvdtdW = \vec{F} \cdot \vec{v} \, dt, a force applied at a point with zero velocity does zero work, regardless of the force's magnitude. Static friction at the contact point therefore contributes nothing to the work-energy balance. This makes D correct: the only external force doing work on the disk is FF acting at the center (which moves with velocity vCv_C), giving the clean result Fs=12mvC2+12ICω2F \cdot s = \frac{1}{2}mv_C^2 + \frac{1}{2}I_C\omega^2. A is wrong because the normal force acts vertically while the contact point has no vertical displacement on a rigid horizontal surface — it does zero work. Introducing a term NδN \cdot \delta conflates rigid-body analysis with contact-deformation models that don't apply here. B is wrong because it treats friction as though it acts at a point moving with the center's velocity ss. That's only true for a sliding (slipping) contact. For rolling without slipping, the contact point is stationary, so friction does no work — not negative work. C is wrong because it invents a fictional cancellation between "translational" and "rotational" work of friction. This is unnecessary and misleading; the correct reason friction does no work is simply that its point of application has zero velocity. Study tip: Always ask yourself "What is the velocity of the point where this force is applied?" before computing work — this single check resolves most rolling-friction work questions instantly.

Question 3

A thin uniform square plate of side aa and mass mm rotates freely (no external torques) about a fixed pivot at one corner. The pivot bearing is frictionless. At time t=0t = 0, the plate is in the horizontal plane with angular velocity ω0\omega_0 about the vertical axis through the pivot corner.

A thin uniform square plate of side aa and mass mm rotates freely (no external torques) about a fixed pivot at one corner. The pivot bearing is frictionless. At time t=0t = 0, the plate is in the horizontal plane with angular velocity ω0\omega_0 about the vertical axis through the pivot corner. Which expression gives the moment of inertia of the square plate about the vertical axis through the pivot corner, and what is the angular momentum about that axis?

  1. Icorner=13ma2I_{\text{corner}} = \dfrac{1}{3}ma^2 and H=13ma2ω0H = \dfrac{1}{3}ma^2\omega_0, obtained by treating the square plate as equivalent to a slender rod of the same mass and length aa rotating about one end, and applying Irod,end=13ma2I_{\text{rod,end}} = \frac{1}{3}ma^2.
  2. Icorner=76ma2I_{\text{corner}} = \dfrac{7}{6}ma^2 and H=76ma2ω0H = \dfrac{7}{6}ma^2\omega_0, obtained by using Icenter=16ma2I_{\text{center}} = \frac{1}{6}ma^2 for the centroidal axis perpendicular to the plate, then applying the parallel-axis theorem with the incorrect distance d=ad = a (full side length) from center to corner, giving Icorner=16ma2+ma2=76ma2I_{\text{corner}} = \frac{1}{6}ma^2 + ma^2 = \frac{7}{6}ma^2.
  3. Icorner=23ma2I_{\text{corner}} = \dfrac{2}{3}ma^2 and H=23ma2ω0H = \dfrac{2}{3}ma^2\omega_0, obtained by summing the moments of inertia of two rectangular halves of the plate about the pivot corner: each half is a rectangle of mass m/2m/2, side aa, and depth a/2a/2, and direct integration about the corner gives 13ma2\frac{1}{3}ma^2 per half, totaling 23ma2\frac{2}{3}ma^2. (correct answer)
  4. Icorner=12ma2I_{\text{corner}} = \dfrac{1}{2}ma^2 and H=12ma2ω0H = \dfrac{1}{2}ma^2\omega_0, obtained by treating the square plate as a thin disk of diameter aa (radius a/2a/2) with I=12mR2=18ma2I = \frac{1}{2}mR^2 = \frac{1}{8}ma^2, then applying the parallel-axis theorem with d=a/2d = a/2, giving 18ma2+14ma2=38ma2\frac{1}{8}ma^2 + \frac{1}{4}ma^2 = \frac{3}{8}ma^2... rounded up to 12ma2\frac{1}{2}ma^2.
Explanation: When finding the moment of inertia of a 2D plate about an out-of-plane axis through a corner, your most reliable approach is the parallel-axis theorem: start from a known centroidal moment of inertia, then shift to the new axis using I=Icm+md2I = I_{cm} + md^2. For a thin square plate, the moment of inertia about the centroidal axis perpendicular to the plate is Icm=16ma2I_{cm} = \frac{1}{6}ma^2. The distance from the center of the square to any corner is the half-diagonal: d=a22d = \frac{a\sqrt{2}}{2}, so d2=a22d^2 = \frac{a^2}{2}. Applying the parallel-axis theorem: Icorner=16ma2+ma22=16ma2+36ma2=23ma2I_{\text{corner}} = \frac{1}{6}ma^2 + m\cdot\frac{a^2}{2} = \frac{1}{6}ma^2 + \frac{3}{6}ma^2 = \frac{2}{3}ma^2. Since there are no external torques, angular momentum is conserved and equals H=Icornerω0=23ma2ω0H = I_{\text{corner}}\,\omega_0 = \frac{2}{3}ma^2\omega_0, confirming C. A is wrong because a square plate is not equivalent to a slender rod — a rod's mass is distributed along one dimension only, whereas the plate extends in two dimensions, giving a larger moment of inertia. B uses the correct centroidal formula but substitutes d=ad = a (the full side length) instead of the true center-to-corner distance d=a22d = \frac{a\sqrt{2}}{2}. This is a classic trap: the center-to-corner distance is the half-diagonal, not the side length. D incorrectly models a square plate as a disk — these shapes have fundamentally different mass distributions and non-interchangeable formulas. Study tip: Always identify the correct centroid-to-axis distance before applying the parallel-axis theorem — for a square, the center-to-corner distance is a22\frac{a\sqrt{2}}{2}, not a2\frac{a}{2} or aa.

Question 4

A uniform slender rod of length L=1.2 mL = 1.2 \text{ m} and mass m=3 kgm = 3 \text{ kg} is pinned at one end (point O) to a fixed wall and released from rest in the horizontal position. As the rod swings downward, a small block of mass M=1.5 kgM = 1.5 \text{ kg} rests on the rod at a distance dd from the pin. The block is free to slide along the rod without friction.

Immediately after release from the horizontal position, what is the minimum distance dd from the pin O at which the block must be placed so that the block does not press against the rod (i.e., the normal force between the block and rod is zero)?

  1. d=2L3=0.80 md = \dfrac{2L}{3} = 0.80 \text{ m}, because at this distance the tangential acceleration of the rod at that point equals gg, meaning the rod accelerates away from the block faster than gravity alone pulls the block downward. (correct answer)
  2. d=3L4=0.90 md = \dfrac{3L}{4} = 0.90 \text{ m}, because at this distance the centripetal acceleration component of the rod point equals gg, satisfying the condition for the block to become weightless relative to the rod surface.
  3. d=L2=0.60 md = \dfrac{L}{2} = 0.60 \text{ m}, because at the midpoint the rod's angular acceleration produces a tangential acceleration equal to the component of gravity along the rod's length, releasing the normal force.
  4. d=3L4=0.90 md = \dfrac{3L}{4} = 0.90 \text{ m}, because the block's weight MgMg adds to the driving torque about O, shifting the critical point outward beyond 2L/32L/3; the heavier the block, the farther from O the critical distance moves.
Explanation: When a pinned rod is released from rest, every point on it undergoes a tangential acceleration (downward, since the rod starts horizontal) given by at=αda_t = \alpha \cdot d, where α\alpha is the angular acceleration. The block, meanwhile, is pulled downward only by gravity gg. If the rod's tangential acceleration at point dd exceeds gg, the rod "falls away" from the block, and the normal force drops to zero. Your goal is to find the minimum dd where at=ga_t = g. For a uniform rod pinned at one end, the rotational equation of motion (using I=13mL2I = \frac{1}{3}mL^2 and torque from gravity acting at the center) gives: α=mgL213mL2=3g2L\alpha = \frac{mg \cdot \frac{L}{2}}{\frac{1}{3}mL^2} = \frac{3g}{2L} Setting the tangential acceleration equal to gg: αd=g    3g2Ld=g    d=2L3\alpha \cdot d = g \implies \frac{3g}{2L} \cdot d = g \implies d = \frac{2L}{3} This confirms answer A is correct. The frictionless block doesn't affect α\alpha because it exerts only a normal (perpendicular) force on the rod — it contributes no torque about O. The mass MM and distance dd are irrelevant to computing α\alpha. Answer B is wrong on two counts: the centripetal acceleration is zero at the instant of release (ω=0\omega = 0), so it can't govern this condition, and 3L/43L/4 is numerically incorrect. Answer C incorrectly identifies the midpoint as critical and confuses "along the rod" with the tangential direction. Answer D is a tempting trap — it sounds physically intuitive that the block's mass shifts the answer, but since the block exerts no torque, it cannot change α\alpha or the critical distance. Study tip: Whenever a block rests on a rotating body without friction, remember it only exerts a normal force — zero torque contribution. Always check whether ω=0\omega = 0 before invoking centripetal terms.

Question 5

In a planar mechanism, crank OA of length r=0.3r = 0.3 m rotates at a constant angular velocity ωOA=10\omega_{OA} = 10 rad/s counterclockwise. The crank is connected by a rigid connecting rod AB of length =0.6\ell = 0.6 m to a slider B that moves along the horizontal x-axis. At the instant when crank OA is horizontal (pointing in the +x+x direction), find the angular velocity of the connecting rod AB.

Using the velocity analysis of the slider-crank mechanism at the instant when OA is horizontal (A is directly to the right of O), which of the following correctly gives ωAB\omega_{AB} and the velocity of slider B?

  1. ωAB=5 rad/s\omega_{AB} = 5 \text{ rad/s} clockwise and vB=3 m/sv_B = 3 \text{ m/s} to the right, obtained by noting that A moves purely upward at vA=ωOAr=3v_A = \omega_{OA} \cdot r = 3 m/s, and since AB is horizontal at this configuration, the vertical component of vAv_A drives rotation of AB while B moves horizontally with vB=vAωABv_B = v_A - \omega_{AB} \cdot \ell.
  2. ωAB=5 rad/s\omega_{AB} = 5 \text{ rad/s} clockwise and vB=0v_B = 0 m/s, obtained by recognizing that when OA is horizontal, A moves vertically upward, and since AB must remain rigid with B constrained to horizontal motion, the only consistent solution is ωAB=vA/=5\omega_{AB} = v_A/\ell = 5 rad/s clockwise and vB=0v_B = 0. (correct answer)
  3. ωAB=0 rad/s\omega_{AB} = 0 \text{ rad/s} and vB=3 m/sv_B = 3 \text{ m/s} to the right, because when OA is horizontal, A moves vertically and AB is horizontal, so the velocity of A relative to B must be purely perpendicular to AB — but AB is horizontal, meaning the perpendicular direction is vertical, which matches vAv_A, requiring ωAB=vA/\omega_{AB} = v_A/\ell and vB=0v_B = 0. This answer reflects the error of setting ωAB=0\omega_{AB} = 0 by confusing the velocity direction constraint.
  4. ωAB=10 rad/s\omega_{AB} = 10 \text{ rad/s} clockwise and vB=3 m/sv_B = 3 \text{ m/s} to the right, obtained by incorrectly applying ωAB=ωOA\omega_{AB} = \omega_{OA} (assuming the connecting rod spins at the same rate as the crank) and computing vBv_B from vA+ωAB×rB/Av_A + \omega_{AB} \times r_{B/A}.
Explanation: Whenever you see a velocity analysis problem for a slider-crank mechanism, your go-to tool is the rigid-body velocity equation: vB=vA+ωAB×rB/A\vec{v}_B = \vec{v}_A + \vec{\omega}_{AB} \times \vec{r}_{B/A}. The key is applying kinematic constraints carefully — B can only move horizontally, and AB is rigid. At the instant OA is horizontal, point A sits directly right of O. Since OA rotates counterclockwise at ωOA=10\omega_{OA} = 10 rad/s, the velocity of A is purely vertical (upward): vA=ωOAr=10×0.3=3v_A = \omega_{OA} \cdot r = 10 \times 0.3 = 3 m/s upward. At this same instant, AB is horizontal, so rB/A\vec{r}_{B/A} points in the +x+x direction. Writing out the velocity equation: vBx^=3j^+ωAB(k^)×(0.6i^)=3j^0.6ωABj^v_B \hat{x} = 3\hat{j} + \omega_{AB}(-\hat{k}) \times (0.6\hat{i}) = 3\hat{j} - 0.6\omega_{AB}\hat{j}. Matching components: the j^\hat{j} equation gives 0=30.6ωAB0 = 3 - 0.6\omega_{AB}, so ωAB=5\omega_{AB} = 5 rad/s clockwise. The i^\hat{i} equation gives vB=0v_B = 0. This confirms B is correct. Choice A gets ωAB\omega_{AB} right but incorrectly computes vB=3v_B = 3 m/s by misapplying the relative velocity formula — it adds rather than properly enforcing the horizontal constraint on B. Choice C sets ωAB=0\omega_{AB} = 0, confusing "the velocity of A is perpendicular to AB" with "AB has no rotation," which is backwards — that perpendicularity is precisely what drives the rotation. Choice D assumes ωAB=ωOA\omega_{AB} = \omega_{OA}, a classic error of treating the connecting rod like it's pinned at a fixed center. Study tip: Always enforce all constraint directions simultaneously. Write out both the i^\hat{i} and j^\hat{j} components — each gives you one equation, and together they uniquely solve for both unknowns.

Question 6

A uniform cylinder of mass mm, radius RR, and moment of inertia IC=12mR2I_C = \frac{1}{2}mR^2 about its center is placed on an inclined plane of angle θ\theta. The coefficient of static friction between the cylinder and the incline is μs\mu_s. The cylinder is released from rest.

What is the minimum value of μs\mu_s required for the cylinder to roll without slipping down the incline, and what is the linear acceleration of the center if rolling without slipping occurs?

  1. μs,min=13tanθ\mu_{s,\min} = \dfrac{1}{3}\tan\theta and a=gsinθa = g\sin\theta, derived by first computing the friction required for rolling and then substituting a=gsinθa = g\sin\theta as the free-sliding acceleration, conflating the rolling and sliding cases.
  2. μs,min=12tanθ\mu_{s,\min} = \dfrac{1}{2}\tan\theta and a=12gsinθa = \dfrac{1}{2}g\sin\theta, derived by incorrectly using the moment of inertia I=mR2I = mR^2 (solid sphere) instead of 12mR2\frac{1}{2}mR^2 in the rotational equation, leading to a different friction requirement and acceleration.
  3. μs,min=23tanθ\mu_{s,\min} = \dfrac{2}{3}\tan\theta and a=13gsinθa = \dfrac{1}{3}g\sin\theta, derived by applying the rotational equation about the contact point and incorrectly including the friction force moment, which double-counts the friction contribution.
  4. μs,min=13tanθ\mu_{s,\min} = \dfrac{1}{3}\tan\theta and a=23gsinθa = \dfrac{2}{3}g\sin\theta, derived by applying Newton's second law for translation and rotation simultaneously and solving for the friction force required, then dividing by the normal force. (correct answer)
Explanation: When a cylinder rolls without slipping, you must apply both Newton's second law for translation and the rotational equation simultaneously — the two are linked by the rolling constraint a=αRa = \alpha R. For translation down the incline: mgsinθf=mamg\sin\theta - f = ma. For rotation about the center: fR=ICα=12mR2aRfR = I_C\alpha = \frac{1}{2}mR^2\cdot\frac{a}{R}, giving f=12maf = \frac{1}{2}ma. Substituting back: mgsinθ12ma=mamg\sin\theta - \frac{1}{2}ma = ma, so a=23gsinθa = \frac{2}{3}g\sin\theta. The required friction force is then f=13mgsinθf = \frac{1}{3}mg\sin\theta. Since the normal force is N=mgcosθN = mg\cos\theta, the minimum static friction coefficient is μs,min=fN=13tanθ\mu_{s,\min} = \frac{f}{N} = \frac{1}{3}\tan\theta. This is exactly D. Choice A makes a conceptual error by plugging in the free-sliding acceleration a=gsinθa = g\sin\theta (no friction case) into the friction equation — it mixes two physically distinct scenarios. Rolling and frictionless sliding are not the same situation, so you cannot borrow that acceleration. Choice B uses I=mR2I = mR^2, which is the moment of inertia for a thin cylindrical shell or hollow cylinder, not a solid cylinder (IC=12mR2I_C = \frac{1}{2}mR^2). Using the wrong II propagates through both the acceleration and friction results. Choice C takes torques about the contact point but incorrectly re-includes the friction moment, effectively double-counting friction's contribution. Taking torques about the contact point should eliminate friction from the equation, not add it twice. Study tip: Always apply the rolling constraint a=αRa = \alpha R to couple your two equations, and keep your moment of inertia formulas straight — confusing solid vs. hollow cylinders is one of the most common traps on dynamics problems.