Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

Consider an object moving according to the position function \(\mathbf{r}(t)=a \cos \omega t \mathbf{i}+a \sin \omega t \mathbf{j}\) If the angular velocity \(\omega\) is halved, by what factor is \(a_{\mathrm{N}}\) changed?

Short Answer

Expert verified
The normal acceleration \(a_N\) is reduced by a factor of 1/4 when the angular velocity \(\omega\) is halved.

Step by step solution

01

Understanding the Position Function

Consider the given position function \(\mathbf{r}(t) = a \cos(\omega t) \mathbf{i} + a \sin(\omega t) \mathbf{j}\). This represents uniform circular motion in a plane with radius 'a' and angular speed '\omega'.
02

Computing the Velocity

The velocity is the derivative of the position function. Differentiate \(\mathbf{r}(t)\) with respect to \(t\). This gives \(\mathbf{v}(t) = -a\omega \sin(\omega t) \mathbf{i} + a\omega \cos(\omega t) \mathbf{j}\).
03

Computing the Acceleration

Acceleration is the derivative of the velocity function. Differentiate \(\mathbf{v}(t)\) with respect to \(t\). This gives \(\mathbf{a}(t) = -a\omega^2 \cos(\omega t) \mathbf{i} - a\omega^2 \sin(\omega t) \mathbf{j}\). By taking the magnitude of acceleration \(a(t)\), we get \(|a(t)| = a\omega^2\). This is the centripetal or radial acceleration.
04

Computing the Normal Acceleration

The normal acceleration \(a_N\) (towards the center of the circle) for circular motion is equal to the magnitude of acceleration \(a(t)\). Accordingly, we get \(a_N = a\omega^2\). As we're interested in the factor by which \(a_N\) changes when \(\omega\) is halved, we need to find \(a_N\) for half of \(\omega\). If we replace \(\omega\) with \(\omega/2\) in the equation, we get \(a_N = a(\omega/2)^2 = a\omega^2/4\). Comparing this to \(a_N = a\omega^2\), we see that \(a_N\) is reduced by 1/4th. The factor by which \(a_N\) is changed when \(\omega\) is halved is 1/4.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

In Exercises 39 and \(40,\) find the angle \(\theta\) between \(r(t)\) and \(r^{\prime}(t)\) as a function of \(t .\) Use a graphing utility to graph \(\theta(t) .\) Use the graph to find any extrema of the function. Find any values of \(t\) at which the vectors are orthogonal. $$ \mathbf{r}(t)=3 \sin t \mathbf{i}+4 \cos t \mathbf{j} $$

The position vector \(r\) describes the path of an object moving in space. Find the velocity, speed, and acceleration of the object. $$ \mathbf{r}(t)=t \mathbf{i}+(2 t-5) \mathbf{j}+3 t \mathbf{k} $$

Find the open interval(s) on which the curve given by the vector-valued function is smooth. $$ \mathbf{r}(t)=\frac{1}{t-1} \mathbf{i}+3 t \mathbf{j} $$

Use the model for projectile motion, assuming there is no air resistance. Use a graphing utility to graph the paths of a projectile for the given values of \(\theta\) and \(v_{0} .\) For each case, use the graph to approximate the maximum height and range of the projectile. (Assume that the projectile is launched from ground level.) (a) \(\theta=10^{\circ}, v_{0}=66 \mathrm{ft} / \mathrm{sec}\) (b) \(\theta=10^{\circ}, v_{0}=146 \mathrm{ft} / \mathrm{sec}\) (c) \(\theta=45^{\circ}, v_{0}=66 \mathrm{ft} / \mathrm{sec}\) (d) \(\theta=45^{\circ}, v_{0}=146 \mathrm{ft} / \mathrm{sec}\) (e) \(\theta=60^{\circ}, v_{0}=66 \mathrm{ft} / \mathrm{sec}\) (f) \(\theta=60^{\circ}, v_{0}=146 \mathrm{ft} / \mathrm{sec}\)

Prove the property. In each case, assume that \(\mathbf{r}, \mathbf{u},\) and \(\mathbf{v}\) are differentiable vector-valued functions of \(t,\) \(f\) is a differentiable real-valued function of \(t,\) and \(c\) is a scalar. If \(\mathbf{r}(t) \cdot \mathbf{r}(t)\) is a constant, then \(\mathbf{r}(t) \cdot \mathbf{r}^{\prime}(t)=0\)

See all solutions

Recommended explanations on Math Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free