Classical MechanicsBSc · Notes

Open a problem for its hint, then reveal the worked solution when needed. Symbols and coordinate conventions follow the corresponding chapter.

Chapter 7

7.1 · Problem 7.1

Hint. Compare its defining sign with the work–energy balance.

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L=T−VL=T-V is the function whose derivatives organize the equations of motion. Mechanical energy is E=T+VE=T+V for the ordinary systems here. For a pendulum, kinetic and potential energy exchange while their sum is constant; their difference generally changes.

7.2 · Problem 7.2

Hint. Use QqδqQ_q\delta q and pqq˙p_q\dot q.

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Angles are dimensionless in SI. Since virtual work is energy, QqQ_q has units N m\mathrm{N\,m}. Since pqq˙p_q\dot q is energy, pqp_q has units kg m2 s−1\mathrm{kg\,m^2\,s^{-1}}: it is an angular-momentum-type quantity.

7.3 · Problem 7.3

Hint. The mass coefficient also changes during the total derivative.

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∂q˙L=m(q)q˙\partial_{\dot q}L=m(q)\dot q, so its total derivative is mq¨+m′q˙2m\ddot q+m^{\prime}\dot q^2. Also ∂qL=12m′q˙2−V′\partial_qL=\tfrac12m^{\prime}\dot q^2-V^{\prime}. Subtraction gives mq¨+12m′q˙2+V′=0m\ddot q+\tfrac12m^{\prime}\dot q^2+V^{\prime}=0. Here m(q)m(q) is an effective inertia coefficient, not a variable-mass particle model.

7.4 · Problem 7.4

Hint. The potential increases with height.

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T=my˙2/2T=m\dot y^2/2, V=mgyV=mgy, and L=my˙2/2−mgyL=m\dot y^2/2-mgy. Hence d(my˙)/dt−(−mg)=0d(m\dot y)/dt-(-mg)=0, giving y¨=−g\ddot y=-g.

7.5 · Problem 7.5

Hint. Linearize only after writing the exact equation.

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From L=ma2θ˙2/2−mga(1−cos⁡θ)L=ma^2\dot\theta^2/2-mga(1-\cos\theta), θ¨+(g/a)sin⁡θ=0\ddot\theta+(g/a)\sin\theta=0. For small angles ω=g/a=10 s−1\omega=\sqrt{g/a}=\sqrt{10}\,\mathrm{s^{-1}}. Thus τ=2π/ω=1.987 s\tau=2\pi/\omega=1.987\,\mathrm s.

7.6 · Problem 7.6

Hint. Both masses contribute to kinetic energy.

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Take qq downward for 5 kg5\,\mathrm{kg}. Then T=4q˙2T=4\dot q^2, V=−2gqV=-2gq, L=4q˙2+2gqL=4\dot q^2+2gq in SI units. The equation is 8q¨=2g8\ddot q=2g, so q¨=g/4=2.45 m s−2\ddot q=g/4=2.45\,\mathrm{m\,s^{-2}}.

7.7 · Problem 7.7

Hint. Keep the factor r2r^2 when differentiating.

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L=m(r˙2+r2θ˙2)/2L=m(\dot r^2+r^2\dot\theta^2)/2. The radial equation is mr¨−mrθ˙2=0m\ddot r-mr\dot\theta^2=0. The angular equation is d(mr2θ˙)/dt=0d(mr^2\dot\theta)/dt=0, or r2θ¨+2rr˙θ˙=0r^2\ddot\theta+2r\dot r\dot\theta=0. These describe a straight line in polar variables.

7.8 · Problem 7.8

Hint. Inspect both partial derivatives.

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V↦V+CV\mapsto V+C changes LL by −C-C. Neither ∂qL\partial_qL nor ∂q˙L\partial_{\dot q}L changes, so neither does the equation. The numerical energy zero shifts by CC.

7.9 · Problem 7.9

Hint. Use y˙=2cxx˙\dot y=2cx\dot x.

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T=12m(1+4c2x2)x˙2T=\tfrac12m(1+4c^2x^2)\dot x^2, V=mgcx2V=mgcx^2. The total velocity derivative is m(1+4c2x2)x¨+8mc2xx˙2m(1+4c^2x^2)\ddot x+8mc^2x\dot x^2, while Lx=4mc2xx˙2−2mgcxL_x=4mc^2x\dot x^2-2mgcx. Thus (1+4c2x2)x¨+4c2xx˙2+2gcx=0(1+4c^2x^2)\ddot x+4c^2x\dot x^2+2gcx=0.

7.10 · Problem 7.10

Hint. Distinguish the reaction from its geometrical effect.

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The rod length is built into x=asin⁡θ,y=−acos⁡θx=a\sin\theta,y=-a\cos\theta, leaving one coordinate. The reaction has zero tangent virtual work and drops from the angular equation. Its geometrical effect remains in T=ma2θ˙2/2T=ma^2\dot\theta^2/2. If needed, the reaction is recovered from radial Newton balance after solving the angular motion.

7.11 · Problem 7.11

Hint. Count the force contributions once.

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No. −∂yV=−mg-\partial_yV=-mg is already included through LL. The right-hand side contains only remaining forces. Including it again would incorrectly double the gravitational acceleration.

7.12 · Problem 7.12

Hint. Check the constraint reaction.

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The equality constraint presumes a taut string. Radial balance gives tension T=maθ˙2+mgcos⁡θ\mathcal T=ma\dot\theta^2+mg\cos\theta. If the predicted tension is negative, the string would need to push, which it cannot do. The string goes slack and the circular-path model must be replaced.

Chapter 8

8.1 · Problem 8.1

Hint. Consider work over a closed forward-and-back path.

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Kinetic friction opposes motion on both legs, so its net work over a closed path is negative. A position potential would give zero net work over that path. Its direction also depends on velocity, not only position.

8.2 · Problem 8.2

Hint. Differentiate the bob position with respect to angle.

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With r=(asin⁡θ,−acos⁡θ)\mathbf r=(a\sin\theta,-a\cos\theta), Qθ=(F,0)⋅(acos⁡θ,asin⁡θ)=Facos⁡θQ_\theta=(F,0)\cdot(a\cos\theta,a\sin\theta)=Fa\cos\theta. Its value vanishes when the permitted tangent is vertical.

8.3 · Problem 8.3

Hint. Use homogeneity in the velocities.

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For quadratic R\mathcal R, ∑iq˙i∂q˙iR=2R\sum_i\dot q_i\partial_{\dot q_i}\mathcal R=2\mathcal R. With Qi=−∂q˙iRQ_i=-\partial_{\dot q_i}\mathcal R, its power is ∑iQiq˙i=−2R\sum_iQ_i\dot q_i=-2\mathcal R. The equality with mechanical-energy change assumes no other drive and no explicit-time energy input.

8.4 · Problem 8.4

Hint. Set the characteristic discriminant to zero.

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The roots of ms2+cs+k=0ms^2+cs+k=0 merge when c2=4mkc^2=4mk. Thus cc=2mk=236=12 kg s−1c_c=2\sqrt{mk}=2\sqrt{36}=12\,\mathrm{kg\,s^{-1}}.

8.5 · Problem 8.5

Hint. Use γ=c/(2m)\gamma=c/(2m).

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γ=1 s−1\gamma=1\,\mathrm{s^{-1}} and ωd=k/m−γ2=3 s−1\omega_d=\sqrt{k/m-\gamma^2}=3\,\mathrm{s^{-1}}. The envelope decays as e−te^{-t} and its oscillation period is 2π/3 s2\pi/3\,\mathrm s.

8.6 · Problem 8.6

Hint. The given coefficient is already a torque coefficient.

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T=ma2θ˙2/2T=ma^2\dot\theta^2/2, V=mga(1−cos⁡θ)V=mga(1-\cos\theta), and Qθ=−bθθ˙Q_\theta=-b_\theta\dot\theta. Therefore ma2θ¨+bθθ˙+mgasin⁡θ=0ma^2\ddot\theta+b_\theta\dot\theta+mga\sin\theta=0. Do not multiply this already angular coefficient by another a2a^2.

8.7 · Problem 8.7

Hint. The stiffness and inertia terms cancel in the amplitude denominator.

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A=F0/(cΩ)=6/(2×3)=1 mA=F_0/(c\Omega)=6/(2\times3)=1\,\mathrm m, within the assumed linear spring model. The phase lag is π/2\pi/2. This is the long-time periodic response, not the entire transient motion.

8.8 · Problem 8.8

Hint. Multiply the equation by velocity.

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mx¨+kx=f(t)−cx˙m\ddot x+kx=f(t)-c\dot x. Multiplication by x˙\dot x gives d[mx˙2/2+kx2/2]/dt=f(t)x˙−cx˙2d[m\dot x^2/2+kx^2/2]/dt=f(t)\dot x-c\dot x^2. The first term can supply or remove energy; the second never supplies it for c>0c>0.

8.9 · Problem 8.9

Hint. Friction now points downward.

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V=−mgqsin⁡αV=-mgq\sin\alpha, T=mq˙2/2T=m\dot q^2/2, and Qq=+μfmgcos⁡αQ_q=+\mu_fmg\cos\alpha while q˙<0\dot q<0. Thus q¨=g(sin⁡α+μfcos⁡α)\ddot q=g(\sin\alpha+\mu_f\cos\alpha). This positive acceleration reduces the upward speed until a new friction regime must be chosen.

8.10 · Problem 8.10

Hint. Retain the transport term in physical velocity.

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va=∑i∂qiraq˙i+∂tra\mathbf v_a=\sum_i\partial_{q_i}\mathbf r_a\dot q_i+\partial_t\mathbf r_a. Dotting with Farem\mathbf F_a^{\rm rem} and summing gives power ∑iQiq˙i+∑aFarem⋅∂tra\sum_iQ_i\dot q_i+\sum_a\mathbf F_a^{\rm rem}\cdot\partial_t\mathbf r_a. The second term is absent only for stationary transformations or when its projection vanishes.

8.11 · Problem 8.11

Hint. The energy theorem includes the remaining forces.

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Although Lt=0L_t=0, E˙=∑iQiq˙i\dot{\mathcal E}=\sum_iQ_i\dot q_i. For viscous drag this is negative. Autonomy implies conservation only when the remaining-force power is also zero.

8.12 · Problem 8.12

Hint. Differentiate the relative velocity with its signs.

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Q1=−c(q˙1−q˙2)Q_1=-c(\dot q_1-\dot q_2) and Q2=+c(q˙1−q˙2)Q_2=+c(\dot q_1-\dot q_2). Their power is −c(q˙1−q˙2)2=−2R-c(\dot q_1-\dot q_2)^2=-2\mathcal R. Equal velocities produce no relative damping force.

Chapter 9

9.1 · Problem 9.1

Hint. Its momentum, not its value, is constrained.

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Yes. For a free particle L=mx˙2/2L=m\dot x^2/2, xx is cyclic but x=x0+vtx=x_0+vt can change. The conserved quantity is px=mvp_x=mv.

9.2 · Problem 9.2

Hint. Write Lagrange’s equation in terms of pip_i.

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p˙i=Lqi+Qi\dot p_i=L_{q_i}+Q_i. Cyclicity sets Lqi=0L_{q_i}=0, leaving p˙i=Qi\dot p_i=Q_i. Momentum is conserved when Qi=0Q_i=0, not from cyclicity alone.

9.3 · Problem 9.3

Hint. Expand the full time derivative and cancel acceleration terms.

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E˙=∑i(q¨ipi+q˙ip˙i)−∑i(Lqiq˙i+Lq˙iq¨i)−Lt\dot{\mathcal E}=\sum_i(\ddot q_ip_i+\dot q_i\dot p_i)-\sum_i(L_{q_i}\dot q_i+L_{\dot q_i}\ddot q_i)-L_t. Since pi=Lq˙ip_i=L_{\dot q_i}, this becomes ∑iq˙i(p˙i−Lqi)−Lt=∑iQiq˙i−Lt\sum_i\dot q_i(\dot p_i-L_{q_i})-L_t=\sum_iQ_i\dot q_i-L_t.

9.4 · Problem 9.4

Hint. Which position is absent?

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xx is absent, and with Qx=0Q_x=0, px=mx˙p_x=m\dot x is conserved. The value of pyp_y generally changes by −V′(y)-V^{\prime}(y).

9.5 · Problem 9.5

Hint. Hold mr2θ˙mr^2\dot\theta fixed.

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θ˙\dot\theta decreases by a factor of four. Tangential speed is vθ=rθ˙=ℓ/(mr)v_\theta=r\dot\theta=\ell/(mr), so it decreases by a factor of two. Radial speed need not follow either rule.

9.6 · Problem 9.6

Hint. The partial time derivative holds x,x˙x,\dot x fixed.

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E=mx˙2/2+k(t)x2/2\mathcal E=m\dot x^2/2+k(t)x^2/2. Since Lt=−k˙x2/2L_t=-\dot kx^2/2 and Q=0Q=0, E˙=k˙x2/2\dot{\mathcal E}=\dot kx^2/2. The actuator changing stiffness exchanges energy.

9.7 · Problem 9.7

Hint. Vary all xax_a by the same constant.

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Translation gives δL=ϵ∑aLxa=0\delta L=\epsilon\sum_aL_{x_a}=0. With unforced Euler–Lagrange equations, Lxa=p˙axL_{x_a}=\dot p_{ax}. Therefore d(∑apax)/dt=0d(\sum_ap_{ax})/dt=0. For ordinary Cartesian kinetic energy this is d(∑amax˙a)/dt=0d(\sum_am_a\dot x_a)/dt=0.

9.8 · Problem 9.8

Hint. Only rotations about the vertical preserve gravity.

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ϕ\phi is cyclic, giving pϕ=ma2sin⁡2θϕ˙=Lzp_\phi=ma^2\sin^2\theta\dot\phi=L_z. Gravity generally exerts a nonzero horizontal torque about the pivot, so the full angular-momentum vector is not constant.

9.9 · Problem 9.9

Hint. Use total momentum divided by total mass.

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P=m(4v)+2m(−v)=2mvP=m(4v)+2m(-v)=2mv. Total mass is 3m3m, so X˙=2v/3\dot X=2v/3, constant in the isolated system. Internal forces can change both individual velocities.

9.10 · Problem 9.10

Hint. Expand the total derivative.

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dL/dt=∑iLqiq˙i+∑iLq˙iq¨i+LtdL/dt=\sum_iL_{q_i}\dot q_i+\sum_iL_{\dot q_i}\ddot q_i+L_t. An autonomous Lagrangian has only the last term zero. The other terms generally do not cancel; for a pendulum, T−VT-V changes as T+VT+V remains fixed.

9.11 · Problem 9.11

Hint. Use δx=−yϵ\delta x=-y\epsilon, δy=xϵ\delta y=x\epsilon.

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Rotational invariance gives 0=∑a[−yaLxa+xaLya−y˙apax+x˙apay]0=\sum_a[-y_aL_{x_a}+x_aL_{y_a}-\dot y_ap_{ax}+\dot x_ap_{ay}]. Replacing Lx,LyL_x,L_y by momentum derivatives combines this into d∑a(xapay−yapax)/dt=0d\sum_a(x_ap_{ay}-y_ap_{ax})/dt=0, which is conservation of LzL_z.

9.12 · Problem 9.12

Hint. Consider a pendulum or an oscillator.

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No. An autonomous spring oscillator conserves mx˙2/2+kx2/2m\dot x^2/2+kx^2/2, but p˙=−kx\dot p=-kx is generally nonzero. Time independence and spatial translation invariance are different symmetries.

Chapter 10

10.1 · Problem 10.1

Hint. Consider transport by a support.

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For moving constraints va=∂tra\mathbf v_a=\partial_t\mathbf r_a when the generalized velocities vanish. Then T=T0=∑ama∣∂tra∣2/2T=T_0=\sum_am_a|\partial_t\mathbf r_a|^2/2, which can be positive. Rest in relative coordinates is not necessarily laboratory rest.

10.2 · Problem 10.2

Hint. Expand the velocity dot product before summing.

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From va=∑ieaiq˙i+wa\mathbf v_a=\sum_i\mathbf e_{ai}\dot q_i+\mathbf w_a, the squared velocity has quadratic, twice-cross, and constant terms. Multiplying by ma/2m_a/2 yields Mij=∑amaeai⋅eajM_{ij}=\sum_am_a\mathbf e_{ai}\cdot\mathbf e_{aj}, bi=∑amaeai⋅wab_i=\sum_am_a\mathbf e_{ai}\cdot\mathbf w_a, and c=∑amawa2/2c=\sum_am_a\mathbf w_a^2/2.

10.3 · Problem 10.3

Hint. Evaluate zTMzz^{\mathsf T}Mz.

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zTMz=∑ama∣∑ieaizi∣2z^{\mathsf T}Mz=\sum_am_a|\sum_i\mathbf e_{ai}z_i|^2. Positive masses make this nonnegative. Regular independent coordinates ensure a nonzero zz moves at least one particle, making it strictly positive. A singular coordinate patch invalidates that last step.

10.4 · Problem 10.4

Hint. Treat A,B,CA,B,C as independent of velocity.

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q˙Tq˙=2Aq˙2+Bq˙\dot qT_{\dot q}=2A\dot q^2+B\dot q, while 2T=2Aq˙2+2Bq˙+2C2T=2A\dot q^2+2B\dot q+2C. They agree only if the lower-degree terms have the required zero contribution, in particular for B=C=0B=C=0.

10.5 · Problem 10.5

Hint. Apply homogeneity separately to each degree.

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∑iq˙ipi=∑iq˙iTq˙i=2T2+T1\sum_i\dot q_ip_i=\sum_i\dot q_iT_{\dot q_i}=2T_2+T_1. Subtracting L=T2+T1+T0−VL=T_2+T_1+T_0-V cancels T1T_1 and leaves T2−T0+VT_2-T_0+V.

10.6 · Problem 10.6

Hint. The transport velocity is perpendicular to the coordinate direction.

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T=m(q˙2+U2)/2T=m(\dot q^2+U^2)/2, so p=mq˙p=m\dot q. Thus H=p2/(2m)−mU2/2H=p^2/(2m)-mU^2/2. The laboratory energy differs by mU2mU^2, a constant in this special case.

10.7 · Problem 10.7

Hint. Inspect the angular inertia coefficient.

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M=diag⁡(m,mr2)M=\operatorname{diag}(m,mr^2) has zero determinant at the origin. All angles describe the same position there, so the chart is not regular. This is not a physical zero mass; Cartesian coordinates remove the singularity.

10.8 · Problem 10.8

Hint. Each cross term contributes to both derivatives.

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p1=m(2q˙1+q˙2)p_1=m(2\dot q_1+\dot q_2) and p2=m(q˙1+3q˙2)p_2=m(\dot q_1+3\dot q_2). The matrix is m(2113)m\begin{pmatrix}2&1\\1&3\end{pmatrix} with determinant 5m2>05m^2>0.

10.9 · Problem 10.9

Hint. Differentiate ∑amava⋅∂qira\sum_am_a\mathbf v_a\cdot\partial_{q_i}\mathbf r_a.

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Tq˙i=∑amava⋅eaiT_{\dot q_i}=\sum_am_a\mathbf v_a\cdot\mathbf e_{ai}. Its time derivative is ∑ama(aa⋅eai+va⋅e˙ai)\sum_am_a(\mathbf a_a\cdot\mathbf e_{ai}+\mathbf v_a\cdot\dot{\mathbf e}_{ai}). Smooth transformations give Tqi=∑amava⋅e˙aiT_{q_i}=\sum_am_a\mathbf v_a\cdot\dot{\mathbf e}_{ai}. Subtracting leaves ∑amaaa⋅∂qira\sum_am_a\mathbf a_a\cdot\partial_{q_i}\mathbf r_a.

10.10 · Problem 10.10

Hint. Expand (U+acos⁡θθ˙)2+(asin⁡θθ˙)2(U+a\cos\theta\dot\theta)^2+(a\sin\theta\dot\theta)^2.

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The cross contribution to TT is maUcos⁡θθ˙maU\cos\theta\dot\theta. Thus T1=maUcos⁡θθ˙T_1=maU\cos\theta\dot\theta, T2=ma2θ˙2/2T_2=ma^2\dot\theta^2/2, and T0=mU2/2T_0=mU^2/2.

10.11 · Problem 10.11

Hint. Symmetry exchanges indices, not coordinate directions.

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No. Symmetry means Mij=MjiM_{ij}=M_{ji}. In polar coordinates Mrr=mM_{rr}=m and Mθθ=mr2M_{\theta\theta}=mr^2, with different dimensions because the coordinates have different dimensions.

10.12 · Problem 10.12

Hint. Apply the product rule to the momentum.

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p=mq˙+B(q)p=m\dot q+B(q), so p˙=mq¨+B′q˙\dot p=m\ddot q+B^{\prime}\dot q. Also Lq=B′q˙−V′L_q=B^{\prime}\dot q-V^{\prime}. Their difference is mq¨+V′m\ddot q+V^{\prime}. In one coordinate this linear term is locally a total derivative of an antiderivative of BB.

Chapter 11

11.1 · Problem 11.1

Hint. Kinetic energy uses laboratory velocity.

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With r(q,t)\mathbf r(q,t), velocity includes ∂tr\partial_t\mathbf r. Omitting it changes TT and can remove the forcing caused by support acceleration. A relative coordinate is allowed, but it must be related to physical position correctly.

11.2 · Problem 11.2

Hint. Set θ¨=0\ddot\theta=0 in the driven angle equation.

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gsin⁡θ0=−Acos⁡θ0g\sin\theta_0=-A\cos\theta_0, giving θ0=−arctan⁡(A/g)\theta_0=-\arctan(A/g) on the downward branch. The bob tilts opposite the support acceleration.

11.3 · Problem 11.3

Hint. Keep the two terms involving X˙θ˙\dot X\dot\theta until subtraction.

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L=ma2θ˙2/2+maX˙cos⁡θθ˙+mX˙2/2−mga(1−cos⁡θ)L=ma^2\dot\theta^2/2+ma\dot X\cos\theta\dot\theta+m\dot X^2/2-mga(1-\cos\theta). Then dLθ˙/dt=ma2θ¨+maX¨cos⁡θ−maX˙sin⁡θθ˙dL_{\dot\theta}/dt=ma^2\ddot\theta+ma\ddot X\cos\theta-ma\dot X\sin\theta\dot\theta and Lθ=−maX˙sin⁡θθ˙−mgasin⁡θL_\theta=-ma\dot X\sin\theta\dot\theta-mga\sin\theta. The cross terms cancel, leaving aθ¨+gsin⁡θ=−X¨cos⁡θa\ddot\theta+g\sin\theta=-\ddot X\cos\theta.

11.4 · Problem 11.4

Hint. Use the sum and difference coordinates.

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The sum obeys s¨+4s=0\ddot s+4s=0, so ωs=2 s−1\omega_s=2\,\mathrm{s^{-1}}. The difference obeys d¨+16d=0\ddot d+16d=0, so ωd=4 s−1\omega_d=4\,\mathrm{s^{-1}}.

11.5 · Problem 11.5

Hint. Calculate its extension.

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When x1=x2x_1=x_2, its extension x2−x1x_2-x_1 is zero at all times. Only the wall springs supply restoring forces, so the frequency is k/m\sqrt{k/m}.

11.6 · Problem 11.6

Hint. Use an azimuth and an angle from the downward vertical.

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x=asin⁡θcos⁡ϕx=a\sin\theta\cos\phi, y=asin⁡θsin⁡ϕy=a\sin\theta\sin\phi, z=−acos⁡θz=-a\cos\theta. The coordinate tangent vectors are perpendicular, with lengths aa and asin⁡θa\sin\theta. Thus T=ma2(θ˙2+sin⁡2θϕ˙2)/2T=ma^2(\dot\theta^2+\sin^2\theta\dot\phi^2)/2.

11.7 · Problem 11.7

Hint. Use Ω2cos⁡θ=g/a\Omega^2\cos\theta=g/a.

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Ω2=9.8/(1×0.5)=19.6 s−2\Omega^2=9.8/(1\times0.5)=19.6\,\mathrm{s^{-2}}, giving Ω=4.43 s−1\Omega=4.43\,\mathrm{s^{-1}}. This is the azimuthal angular speed, not a small-oscillation frequency.

11.8 · Problem 11.8

Hint. Set the right-hand side of its angle equation to zero.

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θ¨=sin⁡θ(Ω2cos⁡θ−g/a)\ddot\theta=\sin\theta(\Omega^2\cos\theta-g/a). Thus θ=0,π\theta=0,\pi modulo 2π2\pi, or cos⁡θ=g/(aΩ2)\cos\theta=g/(a\Omega^2). The off-bottom pair exists only for Ω2≥g/a\Omega^2\geq g/a, with the pair merging at the bottom at equality.

11.9 · Problem 11.9

Hint. Expand the angle equation at zero.

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θ¨≃(Ω2−g/a)θ\ddot\theta\simeq(\Omega^2-g/a)\theta. It is oscillatory for Ω2<g/a\Omega^2<g/a, exponential for Ω2>g/a\Omega^2>g/a, and the linear test is inconclusive at equality. The cubic term there is restoring, −(g/2a)θ3-(g/2a)\theta^3.

11.10 · Problem 11.10

Hint. Look at the surviving support term.

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The Lagrange derivatives cancel the X˙θ˙\dot X\dot\theta terms, leaving only X¨\ddot X. Constant-velocity frames are related by a Galilean transformation. An accelerating support produces relative forcing, equivalent to a fictitious force in its frame.

11.11 · Problem 11.11

Hint. Initial sum and difference are both AA.

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s=Acos⁡(k/m t)s=A\cos(\sqrt{k/m}\,t) and d=Acos⁡((k+2κ)/m t)d=A\cos(\sqrt{(k+2\kappa)/m}\,t). Hence x1=(s+d)/2x_1=(s+d)/2 and x2=(s−d)/2x_2=(s-d)/2. Both frequencies are present even though only one mass was initially displaced.

11.12 · Problem 11.12

Hint. The prescribed rotation has an actuator.

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The motor maintaining Ω\Omega can transfer energy through the moving ideal constraint. The autonomous reduced Lagrangian conserves E=ma2θ˙2/2−ma2Ω2sin⁡2θ/2+V\mathcal E=ma^2\dot\theta^2/2-ma^2\Omega^2\sin^2\theta/2+V, which differs from laboratory T+VT+V.

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