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The shape of the curving slip road joining two motorways that cross at right angles and are at vertical heights \(z=0\) and \(z=h\) can be approximated by the space curve $$ \mathbf{r}=\frac{\sqrt{2} h}{\pi} \ln \cos \left(\frac{z \pi}{2 h}\right) \mathbf{i}+\frac{\sqrt{2} h}{\pi} \ln \sin \left(\frac{z \pi}{2 h}\right) \mathbf{j}+z \mathbf{k} $$ Show that the radius of curvature \(\rho\) of the curve is \((2 h / \pi) \operatorname{cosec}(z \pi / h)\) at height \(z\) and that the torsion \(\tau=-1 / \rho\). (To shorten the algebra, set \(z=2 h \theta / \pi\) and use \(\theta\) as the parameter.)

Short Answer

Expert verified
The radius of curvature at height z is \frac{2h}{\pi} \textrm{cosec}\frac{z\pi}{h}\ and the torsion is \- \frac{1}{\rho}.

Step by step solution

01

Parameterize the Curve

Given the hint to use \(\theta \), set \( z = \frac{2h \theta}{\pi} \). Rewrite the vector equation of the curve in terms of \(\theta \).
02

Compute the Derivative

Find the first derivative of \(\boldsymbol{r}(\theta)\) with respect to \(\theta \).
03

Find the Tangent Vector

Simplify the first derivative to get the tangent vector \(\frac{d\boldsymbol{r}}{d\theta} \).
04

Calculate Velocity Magnitude

Find the magnitude of the tangent vector using the expression for velocity magnitude, \(\big| \frac{d\boldsymbol{r}}{d\theta} \big| \).
05

Compute Second Derivative

Calculate the second derivative of \(\boldsymbol{r}(\theta)\) with respect to \(\theta \).
06

Find the Radius of Curvature

Use the formula \(\rho(\theta) = \frac{ \big| \frac{d\boldsymbol{r}}{d\theta} \big|^3 }{ \big| \frac{d^2\boldsymbol{r}}{d\theta^2} \times \frac{d\boldsymbol{r}}{d\theta} \big| } \). Simplify to show \( \rho = \frac{2h}{\pi} \textrm{cosec}\frac{z\pi}{h}\).
07

Calculate Torsion

Using the result from Step 6, show that the torsion \( \tau = -\frac{1}{\rho} \).

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Radius of Curvature
Understanding the radius of curvature is key in differential geometry, especially for analyzing the shape of curves. The radius of curvature, \(\rho\), measures how sharply a curve bends at a given point. Mathematically, it's defined as the reciprocal of the curvature \(k\), i.e., \(\rho = \frac{1}{k}\).
For the given problem, after parameterizing the curve and computing derivatives, the radius of curvature can be found using the formula:
\[\rho(\theta) = \frac{ | \frac{d\mathbf{r}}{d\theta} |^3 }{ | \frac{d^2\mathbf{r}}{d\theta^2} \times \frac{d\mathbf{r}}{d\theta} | }\]
Using this, we see that for the curve, the radius of curvature at a height \(z\) is: \(\rho = \frac{2h}{\pi} \operatorname{cosec}(\frac{z\pi}{h})\). This means that the tighter the curve (higher \(\operatorname{cosec}\) value), the smaller the radius of curvature.
Torsion
Torsion measures the rate at which a curve twists out of the plane of curvature. It tells you how much the curve deviates from being planar. Mathematically, torsion \(\tau\) is found using the formula:
\[\tau = \frac{ ( \frac{d\boldsymbol{r}}{d\theta} \times \frac{d^2\boldsymbol{r}}{d\theta^2}) \cdot \frac{d^3\boldsymbol{r}}{d\theta^3} }{ | \frac{d\boldsymbol{r}}{d\theta} \times \frac{d^2\boldsymbol{r}}{d\theta^2} |^2}\]
In this problem, the torsion is given by the simpler expression \(\tau = -\frac{1}{\rho}\). This means torsion is inversely related to the radius of curvature, where negative torsion indicates a left-hand twist.
Parametric Curves
Parametric curves express coordinates \(x, y, z\) as functions of a parameter, usually denoted as \(t\) or \((\theta\). These curves are extremely useful for describing complex shapes and motions in space. The differentiable parametric functions help in calculating derivatives, which are crucial for finding tangent vectors, curvatures, and torsions.
In this exercise, the space curve is given by:
\[\mathbf{r} = \frac{\sqrt{2} h}{\pi} \ln(\cos (\frac{z \pi}{2 h})) \mathbf{i} + \frac{\sqrt{2} h}{\pi} \ln(\sin (\frac{z \pi}{2 h})) \mathbf{j} + z \mathbf{k}\].
By substituting \(z = \frac{2h \theta}{\pi}\), it simplifies the equations and computations.
Vector Calculus
Vector calculus is essential for analyzing curves in 3-dimensional space. It involves operations like differentiation and integration of vector fields. Key operations include:
  • Gradient: Measures the rate and direction of change in scalar fields.
  • Divergence: Measures the magnitude of a source or sink at a given point in a vector field.
  • Curl: Measures the rotation of a vector field.
In the context of space curves, vector calculus helps determine the velocity (tangent vector), acceleration, and ultimately the curvature and torsion of the curve.
For instance, the computations in this exercise involve finding the first and second derivatives of the vector \(\mathbf{r}(\theta)\), which are \(\frac{d\mathbf{r}}{d\theta}\) and \(\frac{d^2\mathbf{r}}{d\theta^2}\), respectively.
Space Curves
Space curves are curves that reside in three-dimensional space as opposed to being restricted to a 2D plane. They are described by 3-coordinate functions of a single parameter like \(t\) or \((\theta)\). These curves are crucial in fields such as physics, engineering, and computer graphics.
This exercise deals with a curving slip road represented as a space curve by the vector equation \[\mathbf{r}=\frac{\sqrt{2} h}{\pi} \ln \cos (\frac{z \pi}{2 h}) \mathbf{i}+\frac{\sqrt{2} h}{\pi} \ln \sin (\frac{z \pi}{2 h}) \mathbf{j}+z \mathbf{k}\].
Understanding space curves involves both their curvature and torsion, enabling a comprehensive understanding of their geometry and dynamics.

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Most popular questions from this chapter

Maxwell's equations for electromagnetism in free space (i.e. in the absence of charges, currents and dielectric or magnetic media) can be written (i) \(\nabla \cdot \mathbf{B}=0\) (ii) \(\nabla \cdot \mathbf{E}=0\) (iii) \(\nabla \times \mathbf{E}+\frac{\partial \mathbf{B}}{\partial t}=\mathbf{0}\) (iv) \(\nabla \times \mathbf{B}-\frac{1}{c^{2}} \frac{\partial \mathbf{E}}{\partial t}=\mathbf{0}\). A vector \(\mathbf{A}\) is defined by \(\mathbf{B}=\nabla \times \mathbf{A}\), and a scalar \(\phi\) by \(\mathbf{E}=-\nabla \phi-\partial \mathbf{A} / \partial t\). Show that if the condition (v) \(\nabla \cdot \mathbf{A}+\frac{1}{c^{2}} \frac{\partial \phi}{\partial t}=0\) is imposed (this is known as choosing the Lorenz gauge), then both \(\mathbf{A}\) and \(\phi\) satisfy the wave equations (vi) \(\nabla^{2} \phi-\frac{1}{c^{2}} \frac{\partial^{2} \phi}{\partial t^{2}}=0\), (vii) \(\quad \nabla^{2} \mathbf{A}-\frac{1}{c^{2}} \frac{\partial^{2} \mathbf{A}}{\partial t^{2}}=\mathbf{0}\) The reader is invited to proceed as follows. (a) Verify that the expressions for \(\mathbf{B}\) and \(\mathbf{E}\) in terms of \(\mathbf{A}\) and \(\phi\) are consistent with (i) and (iii). (b) Substitute for \(\mathbf{E}\) in (ii) and use the derivative with respect to time of \((v)\) to eliminate \(\mathbf{A}\) from the resulting expression. Hence obtain (vi). (c) Substitute for \(\mathbf{B}\) and \(\mathbf{E}\) in (iv) in terms of \(\mathbf{A}\) and \(\phi .\) Then use the divergence of (v) to simplify the resulting equation and so obtain (vii).

In a Cartesian system, \(A\) and \(B\) are the points \((0,0,-1)\) and \((0,0,1)\) respectively. In a new coordinate system a general point \(P\) is given by \(\left(u_{1}, u_{2}, u_{3}\right)\) with \(u_{1}=\frac{1}{2}\left(r_{1}+r_{2}\right), u_{2}=\frac{1}{2}\left(r_{1}-r_{2}\right), u_{3}=\phi ;\) here \(r_{1}\) and \(r_{2}\) are the distances \(A P\) and \(B P\) and \(\phi\) is the angle between the plane \(A B P\) and \(y=0\). (a) Express \(z\) and the perpendicular distance \(\rho\) from \(P\) to the \(z\)-axis in terms of \(u_{1}, u_{2}, u_{3}\) (b) Evaluate \(\partial x / \partial u_{i}, \partial y / \partial u_{i}, \partial z / \partial u_{i}\), for \(i=1,2,3\). (c) Find the Cartesian components of \(\hat{\mathbf{u}}_{j}\) and hence show that the new coordinates are mutually orthogonal. Evaluate the scale factors and the infinitesimal volume element in the new coordinate system. (d) Determine and sketch the forms of the surfaces \(u_{i}=\) constant. (e) Find the most general function \(f\) of \(u_{1}\) only that satisfies \(\nabla^{2} f=0\)

For a description in spherical polar coordinates with axial symmetry of the flow of a very viscous fluid, the components of the velocity field \(\mathbf{u}\) are given in terms of the stream function \(\psi\) by $$ u_{r}=\frac{1}{r^{2} \sin \theta} \frac{\partial \psi}{\partial \theta}, \quad u_{\theta}=\frac{-1}{r \sin \theta} \frac{\partial \psi}{\partial r} $$ Find an explicit expression for the differential operator \(E\) defined by $$ E \psi=-(r \sin \theta)(\nabla \times \mathbf{u})_{\phi} $$ The stream function satisfies the equation of motion \(E^{2} \psi=0\) and, for the flow of a fluid past a sphere, takes the form \(\psi(r, \theta)=f(r) \sin ^{2} \theta\). Show that \(f(r)\) satisfies the (ordinary) differential equation $$ r^{4} f^{(4)}-4 r^{2} f^{\prime \prime}+8 r f^{\prime}-8 f=0 $$

In a magnetic field, field lines are curves to which the magnetic induction \(\mathbf{B}\) is everywhere tangential. By evaluating \(d \mathbf{B} / d s\), where \(s\) is the distance measured along a field line, prove that the radius of curvature at any point on a line is given by $$ \rho=\frac{B^{3}}{|\mathbf{B} \times(\mathbf{B} \cdot \nabla) \mathbf{B}|} $$

If two systems of coordinates with a common origin \(O\) are rotating with respect to each other, the measured accelerations differ in the two systems. Denoting by \(\mathbf{r}\) and \(\mathbf{r}^{\prime}\) position vectors in frames \(O X Y Z\) and \(O X^{\prime} Y^{\prime} Z^{\prime}\) respectively, the connection between the two is $$ \ddot{\mathbf{r}}^{\prime}=\ddot{\mathbf{r}}+\dot{\omega} \times \mathbf{r}+2 \omega \times \dot{\mathbf{r}}+\omega \times(\omega \times \mathbf{r}) $$ where \(\omega\) is the angular velocity vector of the rotation of \(O X Y Z\) with respect to \(O X^{\prime} Y^{\prime} Z^{\prime}\) (taken as fixed). The third term on the RHS is known as the Coriolis acceleration, whilst the final term gives rise to a centrifugal force. Consider the application of this result to the firing of a shell of mass \(m\) from a stationary ship on the steadily rotating earth, working to the first order in \(\omega\left(=7.3 \times 10^{-5} \mathrm{rad} \mathrm{s}^{-1}\right)\). If the shell is fired with velocity \(\mathbf{v}\) at time \(t=0\) and only reaches a height that is small compared to the radius of the earth, show that its acceleration, as recorded on the ship, is given approximately by $$ \ddot{\mathbf{r}}=\mathbf{g}-2 \omega \times(\mathbf{v}+\mathbf{g} t) $$ where \(m \mathbf{g}\) is the weight of the shell measured on the ship's deck. The shell is fired at another stationary ship (a distance \(\mathbf{s}\) away) and \(\mathbf{v}\) is such that the shell would have hit its target had there been no Coriolis effect. (a) Show that without the Coriolis effect the time of flight of the shell would have been \(\tau=-2 \mathbf{g} \cdot \mathbf{v} / g^{2}\) (b) Show further that when the shell actually hits the sea it is off target by approximately $$ \frac{2 \tau}{g^{2}}[(\mathbf{g} \times \omega) \cdot \mathbf{v}](\mathbf{g} \tau+\mathbf{v})-(\omega \times \mathbf{v}) \tau^{2}-\frac{1}{3}(\omega \times \mathbf{g}) \tau^{3} $$ (c) Estimate the order of magnitude \(\Delta\) of this miss for a shell for which \(v=300\) \(\mathrm{m} \mathrm{s}^{-1}\), firing close to its maximum range ( \(\mathbf{v}\) makes an angle of \(\pi / 4\) with the vertical) in a northerly direction, whilst the ship is stationed at latitude \(45^{\circ}\) North.

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