Problem 114
Question
Solve each problem. Suppose an airplane flying faster than sound goes directly over you. Assume that the plane is flying at a constant altitude. At the instant you feel the sonic boom from the plane, the angle of elevation to the plane is $$\alpha=2 \arcsin \frac{1}{m}$$ where \(m\) is the Mach number of the plane's speed. (The Mach number is the ratio of the speed of the plane to the speed of sound.) Find \(\alpha\) to the nearest degree for each value of \(m\) (a) \(m=1.2\) (b) \(m=1.5\) (c) \(m=2\) (d) \(m=2.5\)
Step-by-Step Solution
Verified Answer
(a) 113°, (b) 84°, (c) 60°, (d) 47°.
1Step 1: Understand the Formula for \( \alpha \)
To find the angle of elevation \( \alpha \), we use the formula \( \alpha = 2 \arcsin \frac{1}{m} \), where \( m \) is the Mach number. This tells us the angle at which the sonic boom is heard when a plane moves faster than the speed of sound.
2Step 2: Calculate \( \alpha \) for \( m = 1.2 \)
Substitute \( m = 1.2 \) into the formula: \( \alpha = 2 \arcsin \frac{1}{1.2} \). Calculate \( \frac{1}{1.2} = 0.8333 \). Find \( \arcsin(0.8333) \approx 56.44^\circ \). Therefore, \( \alpha = 2 \times 56.44^\circ \approx 112.88^\circ \). Round to the nearest degree: \( \alpha = 113^\circ \).
3Step 3: Calculate \( \alpha \) for \( m = 1.5 \)
Substitute \( m = 1.5 \) into the formula: \( \alpha = 2 \arcsin \frac{1}{1.5} \). Calculate \( \frac{1}{1.5} = 0.6667 \). Find \( \arcsin(0.6667) \approx 41.81^\circ \). Therefore, \( \alpha = 2 \times 41.81^\circ \approx 83.62^\circ \). Round to the nearest degree: \( \alpha = 84^\circ \).
4Step 4: Calculate \( \alpha \) for \( m = 2 \)
Substitute \( m = 2 \) into the formula: \( \alpha = 2 \arcsin \frac{1}{2} \). Calculate \( \frac{1}{2} = 0.5 \). Find \( \arcsin(0.5) = 30^\circ \). Therefore, \( \alpha = 2 \times 30^\circ = 60^\circ \). No rounding needed: \( \alpha = 60^\circ \).
5Step 5: Calculate \( \alpha \) for \( m = 2.5 \)
Substitute \( m = 2.5 \) into the formula: \( \alpha = 2 \arcsin \frac{1}{2.5} \). Calculate \( \frac{1}{2.5} = 0.4 \). Find \( \arcsin(0.4) \approx 23.58^\circ \). Therefore, \( \alpha = 2 \times 23.58^\circ \approx 47.16^\circ \). Round to the nearest degree: \( \alpha = 47^\circ \).
Key Concepts
Mach NumberAngle of ElevationSonic BoomArcsine Function
Mach Number
The Mach number is a dimensionless quantity representing the speed of an object relative to the speed of sound in the surrounding medium. It is named after the Austrian physicist Ernst Mach. Understanding the Mach number is crucial in aviation and aerospace engineering when dealing with high-speed travel such as supersonic and hypersonic flights. Here are some key aspects:
- A Mach number of 1 indicates the speed of sound.
- Supersonic speeds are greater than Mach 1.
- A Mach number less than 1 signifies the object is moving slower than sound.
Angle of Elevation
The angle of elevation is the angle between the horizontal line from the observer and the line of sight to an object above the horizontal. It is a common application in trigonometry used to determine heights and distances indirectly. Here’s how you can think about it:
- It is measured upwards from the horizontal.
- Commonly used in problems involving heights and distances.
Sonic Boom
A sonic boom is a loud sound associated with the shock waves created when an object exceeds the speed of sound. This phenomenon is why you sometimes hear a sudden explosive noise when jets fly overhead at high speeds. Here’s what happens during a sonic boom:
- Air pressure waves build up around the object as it travels at supersonic speeds.
- The pressure from the shock waves creates the explosive sound.
- It's often compared to the sound of thunder during a storm.
Arcsine Function
The arcsine function is one of the inverse trigonometric functions, often denoted as \(\arcsin\). It is the inverse of the sine function, providing the angle that corresponds to a given sine value. Key points include:
- Its range is from \(-\frac{\pi}{2}\) to \(\frac{\pi}{2}\).
- It is typically used to calculate angles from given ratios.
Other exercises in this chapter
Problem 112
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