Chapter 6: Problem 77
Verify the identity. $$\tan \left(\sin ^{-1} \frac{x-1}{4}\right)=\frac{x-1}{\sqrt{16-(x-1)^{2}}}$$
/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none}
Learning Materials
Features
Discover
Chapter 6: Problem 77
Verify the identity. $$\tan \left(\sin ^{-1} \frac{x-1}{4}\right)=\frac{x-1}{\sqrt{16-(x-1)^{2}}}$$
All the tools & learning materials you need for study success - in one app.
Get started for free
Use the half-angle formulas to simplify the expression. $$-\sqrt{\frac{1-\cos (x-1)}{2}}$$
(a) plot the points, (b) find the distance between the points, and (c) find the midpoint of the line segment connecting the points. $$(-4,-3),(6,10)$$
Find the exact values of \(\sin (u / 2), \cos (u / 2),\) and \(\tan (u / 2)\) using the half-angle formulas. $$\tan u=-\frac{5}{12}, \quad 3 \pi / 2
The Mach number \(M\) of an airplane is the ratio of its speed to the speed of sound. When an airplane travels faster than the speed of sound, the sound waves form a cone behind the airplane (see figure). The Mach number is related to the apex angle \(\theta\) of the cone by $$\sin \frac{\theta}{2}=\frac{1}{M}$$ (a) Find the angle \(\theta\) that corresponds to a Mach number of 1. (b) Find the angle \(\theta\) that corresponds to a Mach number of 4.5 (c) The speed of sound is about 760 miles per hour. Determine the speed of an object having the Mach numbers in parts (a) and (b). (d) Rewrite the equation as a trigonometric function of \(\theta\).
Find the exact values of \(\sin (u / 2), \cos (u / 2),\) and \(\tan (u / 2)\) using the half-angle formulas. $$\sec u=\frac{7}{2}, \quad 0
What do you think about this solution?
We value your feedback to improve our textbook solutions.