Problems

A hollow spherical ball of mass \(M\) and radius \(r\) runs between two horizontal parallel bars a distance \(2d\) apart and at the same height. The coefficient of friction between the ball and the bars is \(\mu\). Initially the ball rolls without slipping along the bars with constant velocity \(v\), but it then collides with an obstacle in the form of a smooth, perfectly elastic, fixed vertical wall at right angles to the direction of motion of the ball. Describe carefully the subsequent motion of the ball. What is the total work done by the frictional forces? [The moment of inertia of the ball about its diameter is \(\frac{2}{3}Mr^2\).]

An elliptical disc with semi-axes \(a, b\) can be thought of as a circular disc of radius \(b\) which has been stretched uniformly by a factor \(a/b\) in one direction and not stretched in the perpendicular direction. Use this concept (or any other method) to show that the radius of gyration of an elliptical disc about an axis through its centre perpendicular to its plane is \(\frac{1}{2}\sqrt{a^2+b^2}\). The disc is at rest on a flat table with its major axis vertical. Given an infinitesimal push, it rolls sideways without slipping. Find its angular velocity when the minor axis is vertical.

Two stars \(B\) and \(X\) with masses \(m_B\) and \(m_X\) and separation \(d\) revolve in circles around their common centre of gravity, under the influence of Newtonian gravity (force of attraction \(= Gm_Bm_X/d^2\)). Find the velocity of each star and the period of revolution. An observer views the system from a very large distance at an angle \(\theta\) to the normal to the plane of their orbits. He can recognise \(B\) as a star of a type that has mass \(m_B\), and star \(X\), which produces X-rays must be either a neutron star or a black hole, whose mass is less than or more than 2 units respectively. He measures the line-of-sight component of \(B\)'s velocity, and finds it fits a curve \(V = K\sin \omega t\). Show that \[\frac{m_X^3}{(m_B+m_X)^2}\sin^3\theta = \frac{|K|^3}{\omega G}.\] His measurements give \(\frac{K^3}{\omega G} = 1/250\) units. If all values of \(\cos\theta\) are equally likely, find the probability that \(X\) is a black hole.

A particle can slide smoothly in a uniform straight tube. The tube and the particle have equal masses. The tube can rotate freely in a horizontal plane about a fixed end. It is given an initial angular velocity, and the particle is displaced slightly along the tube from its fixed end. Show that the particle must eventually leave the other end, and does so at an angle of approximately \(\tan^{-1}\frac{1}{2}\) to the axis of the tube.

A heavy rod \(AB\) slides by means of smooth rings on the two fixed rods \(CD, CE\) which lie in a vertical plane and make acute angles \(\alpha, \beta\) respectively with the horizontal (see the diagram below). The centre of gravity of the rod \(AB\) is at a fraction \(\lambda\) of its length from \(B\). If the rod makes an angle \(\theta\) with the vertical, show that in equilibrium \[\cot\theta = \lambda\cot\beta-(1-\lambda)\cot\alpha.\] Show that the equilibrium is always stable when \(A\) and \(B\) lie below \(C\).

+ - ↺

A spacecraft has cylindrical symmetry. The unit vector through the centre of gravity along the axis of symmetry is \(\mathbf{l}\) and the spin vector of the spacecraft is \(\boldsymbol{\omega}\). The spacecraft is falling freely in space so that the equation of motion of its axis of symmetry is \[\frac{d\mathbf{l}}{dt} = \boldsymbol{\omega} \times \mathbf{l}.\] Show that \(\boldsymbol{\omega} = \mathbf{l} \times \frac{d\mathbf{l}}{dt} + (\boldsymbol{\omega} \cdot \mathbf{l})\mathbf{l}\). The angular momentum \(\mathbf{h}\) of the spacecraft may be written \[\mathbf{h} = A\mathbf{l} \times \frac{d\mathbf{l}}{dt} + C(\boldsymbol{\omega} \cdot \mathbf{l})\mathbf{l}, \quad \text{where \(A\) and \(C\) are constants.}\] The craft is struck by a meteor and the angular momentum after this impact is \(\Gamma\mathbf{k}\), where \(\Gamma\) is a constant and \(\mathbf{k}\) a constant unit vector. Show that \[\frac{\boldsymbol{\omega}}{\Gamma} = \frac{\mathbf{l} \times (\mathbf{k} \times \mathbf{l})}{A} + \frac{(\mathbf{k} \cdot \mathbf{l})\mathbf{l}}{C}\] and that \[\frac{d\mathbf{l}}{dt} = \frac{\Gamma}{A}\mathbf{k} \times \mathbf{l}.\] Deduce the subsequent motion of the spacecraft's axis. [You may assume that \(\mathbf{a} \times (\mathbf{b} \times \mathbf{c}) = (\mathbf{a} \cdot \mathbf{c})\mathbf{b} - (\mathbf{a} \cdot \mathbf{b})\mathbf{c}\).]