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A jet plane flies overhead at Mach 1.70 and at a constant altitude of 1250 m. (a) What is the angle a of the shock-wave cone? (b) How much time after the plane passes directly overhead do you hear the sonic boom? Neglect the variation of the speed of sound with altitude.

Short Answer

Expert verified
(a) 36.0° (b) 6.2 s

Step by step solution

01

Understanding Mach number and angle of the shock-wave cone

Mach number is defined as the ratio of the speed of an object to the speed of sound in the same medium. Therefore, when a jet is flying at Mach 1.70, it is moving at 1.70 times the speed of sound. The angle of the shock wave cone, or Mach angle \( \theta \), is determined using the formula: \( \sin(\theta) = \frac{1}{\text{Mach number}} \).
02

Calculating the angle of the shock-wave cone

Using the formula \( \sin(\theta) = \frac{1}{\text{Mach number}} \) and substituting the Mach number: \( \sin(\theta) = \frac{1}{1.70} \). Calculating this gives \( \theta \approx \sin^{-1}(0.5882) \), which results in \( \theta \approx 36.0^{\circ} \).
03

Defining parameters for the sonic boom time calculation

The altitude of the plane is given as 1250 m. Assuming the speed of sound \( v \) is approximately 343 m/s (at 20 degrees Celsius), consider the right-triangle formed by the vertical height (altitude) and the hypotenuse (which extends to the point where the sound first reaches the ground).
04

Time calculation from the hypotenuse

The time \( t \) it takes for the sound to reach the ground is found by dividing the distance of the hypotenuse by the speed of sound. The hypotenuse is \( \frac{1250}{\sin(36.0^{\circ})} \) m, resulting in \( \approx 2126 \, m \). Calculate \( t = \frac{2126 \, m}{343 \, m/s} \approx 6.2 \, s \).

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Key Concepts

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

Mach Number
The Mach number is a dimensionless quantity used to express the ratio of an object's speed to the speed of sound in the medium it travels through. It is a vital concept in aerodynamics, especially when dealing with objects moving at high velocities, like aircraft. For example, when a jet is traveling at Mach 1.70, it indicates that the jet's speed is 1.70 times faster than the speed of sound in the surrounding air.

Calculating the Mach number helps determine how fast an object is moving relative to the speed of sound. This information is crucial for understanding shock waves and other aerodynamic phenomena that occur at high speeds.

To illustrate, when an aircraft surpasses the speed of sound (i.e., Mach 1), it begins to form a conical shock wave, creating a "shock wave cone" with an angle. The precise angle of this cone can be calculated using the equation: \( \sin(\theta) = \frac{1}{\text{Mach number}} \).

Understanding the Mach number not only aids in computing this angle but also serves as a benchmark that informs engineers and scientists about the aerodynamic challenges and behaviors that are encountered at different speeds.
Sonic Boom
A sonic boom is a loud noise associated with the shock waves created when an object travels through the air at a speed faster than sound. This phenomenon occurs when an object, like a jet plane, moves at supersonic speeds, meaning it has surpassed the speed of sound.

When an aircraft reaches this critical speed, the air cannot move out of the way quickly enough, leading to a rapid compression of air and the formation of shock waves. These shock waves travel to the ground and are perceived as a sonic boom to those nearby.
  • The sonic boom is an audible signal that the aircraft has broken the sound barrier.
  • This boom can be startling and is often described as a loud thunderclap.
  • The loudness is due to the sudden change in air pressure as a shock wave passes by an observer.
The time it takes for the sonic boom to be heard after a plane has passed overhead depends on the altitude of the aircraft and the speed of sound in the atmosphere. In our exercise, after the plane flies at 1250 meters overhead, the sonic boom is heard approximately 6.2 seconds later.
Speed of Sound
The speed of sound refers to the velocity at which sound waves travel through a given medium. In air, this speed is influenced by factors such as temperature, altitude, and humidity, with a typical speed of approximately 343 meters per second (m/s) at 20 degrees Celsius at sea level.

Several critical aspects affect the speed of sound:
  • Temperature: As the temperature increases, air molecules move faster, increasing the speed of sound.
  • Altitude: Higher altitudes typically see a slower speed of sound due to thinner air.
  • Humidity: An increase in humidity usually raises the speed of sound since moist air is less dense than dry air.
In calculations involving the speed of sound, we often assume a constant speed for simplicity, such as in the provided exercise. Here, a speed of 343 m/s was used, assuming standard conditions.

This constant helps in making quick calculations for determining factors like the time delay before hearing a sonic boom, as seen when assessing how long after a jet passes overhead its sonic boom is heard. Understanding and accounting for the speed of sound is fundamental in aerodynamics and various other applications ranging from meteorology to audio engineering.

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