\({ }^{\dagger} \mathrm{A}\) small bead is threaded on a smooth wire in the shape of a curve given parametrically by \(\boldsymbol{r}=\boldsymbol{r}(q)\). The wire rotates with constant angular velocity about a vertical axis. Show that $$ \frac{\mathrm{d}}{\mathrm{d} t}\left[\frac{1}{2} \dot{q}^{2} \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \cdot \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q}\right]=\dot{q} \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \cdot \ddot{\boldsymbol{r}} $$ where the dot is the time derivative relative to a frame rotating with the wire, and \(\boldsymbol{r}\) is measured from an origin on the axis Deduce that $$ \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \cdot \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \dot{q}^{2}-(\boldsymbol{\omega} \wedge \boldsymbol{r}) \cdot(\boldsymbol{\omega} \wedge \boldsymbol{r})-2 \boldsymbol{g} \cdot \boldsymbol{r}=\text { constant. } $$ Does this result still hold when the axis of rotation is not vertical?

Short Answer

Expert verified
To summarize the solution, we took the time derivative of the given expression and simplified it using the chain rule, product rule, and other derivative properties. We then deduced the second given equation by relating centripetal acceleration and gravitational acceleration using the position vector and its derivatives. Finally, we discussed that the result may not hold true when the axis of rotation is not vertical, as centripetal acceleration would have components acting in multiple directions in that case.

Step by step solution

01

Calculate the time derivative

We have to find the time derivative of: $$\frac{1}{2} \dot{q}^{2} \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \cdot \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q}$$ Using the product rule for derivatives and the chain rule, we get: $$\frac{\mathrm{d}}{\mathrm{d} t}\left[\frac{1}{2} \dot{q}^{2} \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \cdot \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q}\right] = \dot{q} \ddot{q} \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \cdot \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} + \frac{1}{2} \dot{q}^{2} \frac{\mathrm{d}^{2} \boldsymbol{r}}{\mathrm{d} t \mathrm{d} q} \cdot \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q}$$ #Step 2: Simplify the expression#
02

Simplify the time derivative

Since \(\frac{\mathrm{d}^{2} \boldsymbol{r}}{\mathrm{d} t \mathrm{d} q} = \frac{\mathrm{d}}{\mathrm{d} q} \left( \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} t} \right)\), the second term can be rewritten as: $$\frac{1}{2} \dot{q}^{2} \frac{\mathrm{d}}{\mathrm{d} q} \left( \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} t} \right) \cdot \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} = \frac{1}{2} \dot{q}^{2} \frac{\mathrm{d}}{\mathrm{d} q} \left( \dot{\boldsymbol{r}} \right) \cdot \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q}$$ Now, using the product rule for derivatives, we get: $$\frac{1}{2} \dot{q}^{2} \frac{\mathrm{d}}{\mathrm{d} q} \left( \dot{\boldsymbol{r}} \right) \cdot \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} = \dot{q} \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \cdot \ddot{\boldsymbol{r}}$$ Thus, we have: $$\frac{\mathrm{d}}{\mathrm{d} t}\left[\frac{1}{2} \dot{q}^{2} \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \cdot \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q}\right] = \dot{q} \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \cdot \ddot{\boldsymbol{r}}$$ #Step 3: Deduce the second equation#
03

Deduce the given equation

We know that the centripetal acceleration of the bead is given by: $$(\boldsymbol{\omega} \wedge \boldsymbol{r}) \cdot (\boldsymbol{\omega} \wedge \boldsymbol{r}) = \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \cdot \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \dot{q}^{2}$$ Also, the gravitational acceleration is given by: $$\boldsymbol{g} \cdot \boldsymbol{r} = - \frac{1}{2} \mathrm{d^{2} r^{2}}{\mathrm{d} t^{2}}$$ Rearranging these two equations and adding them together, we get: $$\frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \cdot \frac{\mathrm{d} \boldsymbol{r}}{\mathrm{d} q} \dot{q}^{2} - (\boldsymbol{\omega} \wedge \boldsymbol{r}) \cdot (\boldsymbol{\omega} \wedge \boldsymbol{r}) - 2 \boldsymbol{g} \cdot \boldsymbol{r} = \text{constant}$$ #Step 4: Discuss the result for non-vertical axis of rotation#
04

Non-vertical axis of rotation case

In the case where the axis of rotation is not vertical, we can no longer claim that the centripetal acceleration and gravitational acceleration remain separate as in the previous step. Since centripetal acceleration now has components acting in multiple directions, the equation may not hold true for a more general case.

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Most popular questions from this chapter

Two frames \(R\) and \(\tilde{R}\) are moving relative to each other without rotation. A particle has kinetic energy \(T\) measured in \(R\) and \(\tilde{T}\) measured in \(\widetilde{R}\). Show that $$ T=\tilde{T}+\boldsymbol{u} \cdot \boldsymbol{p}+c $$ where \(\boldsymbol{p}=m \boldsymbol{v}\) is the momentum of the particle measure in \(R, \boldsymbol{u}\) is the velocity of \(\tilde{R}\) relative to \(R\), and \(c\) is a constant.

Show that the motion of a rigid body is determined at any instant by the velocities of three non-collinear points. Three particles \(A, B\), and \(C\) have velocities \(\boldsymbol{u}, \boldsymbol{v}\), and \(\boldsymbol{w}\) respectively relative to a frame \(R\). Show that they can belong to a rigid body if and only if $$ (a-b) \cdot(u-v)=(b-c) \cdot(v-w)=(c-a) \cdot(w-u)=0 $$ where \(\boldsymbol{a}, \boldsymbol{b}\), and \(\boldsymbol{c}\) are the position vectors of \(A, B\), and \(C\) from the origin of \(R\).

Show that if \(H\) is a proper orthogonal matrix such that \(H_{33}=1\), then there is a unique angle \(\alpha \in[0,2 \pi)\) such that $$ H=\left(\begin{array}{ccc} \cos \alpha & \sin \alpha & 0 \\ -\sin \alpha & \cos \alpha & 0 \\ 0 & 0 & 1 \end{array}\right) $$ Show that if \(H_{33}=-1\), then there is a unique angle \(\alpha \in[0,2 \pi)\) such that $$ H=\left(\begin{array}{ccc} -\cos \alpha & -\sin \alpha & 0 \\ -\sin \alpha & \cos \alpha & 0 \\ 0 & 0 & -1 \end{array}\right) $$ Sketch a diagram of two orthonormal triads with this transition matrix, showing the angle \(\alpha\).

A sphere of radius \(a\) is rolling without slipping on a rough horizontal plane in such a way that its centre traces out a horizontal circle, radius \(b\) and centre \(O\), with constant angular speed \(\Omega\). Let \((i, j, k)\) be an orthonormal triad with \(k\) vertical and \(i\) in the direction from \(O\) to the centre of the sphere. Show that the angular velocity of the sphere relative to the plane satisfies $$ \boldsymbol{\omega}=n \boldsymbol{k}-\frac{b}{a} \Omega i $$ where \(n=\boldsymbol{\omega} \cdot \boldsymbol{k}\). Show that if \(n\) is constant, then the locus of the point of contact on the sphere is a circle. What is its radius?

Suppose that the matrix \(H\) in \((1.5)\) is given by $$ H=\frac{1}{\sqrt{6}}\left(\begin{array}{ccc} \sqrt{2} & \sqrt{2} & \sqrt{2} \\ -2 & 1 & 1 \\ 0 & -\sqrt{3} & \sqrt{3} \end{array}\right) $$ Check that \(H^{\mathrm{t}} H=H H^{\mathrm{t}}=I\). Write down the components of \(\boldsymbol{e}_{1}\), \(e_{2}\), and \(e_{3}\) in \(\tilde{T}\), and the components of \(\tilde{e}_{1}, \tilde{e}_{2}\), and \(\tilde{e}_{3}\) in \(\mathcal{T}\).

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