/*! 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} Problem 4 The Chevrolet Camaro shown in Fi... [FREE SOLUTION] | 91Ó°ÊÓ

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The Chevrolet Camaro shown in Figure 10.29 has a mass of \(2500 \mathrm{~kg}\), a drag coefficient of \(0.25,\) and a frontal area of \(1.2 \mathrm{~m}^{2} .\) The car deploys a \(2.2-\mathrm{m}\) -diameter parachute to slow down from an initial velocity of \(110 \mathrm{~m} / \mathrm{s},\) and the drag coefficient of the parachute is 1.5. Assuming \(C_{\mathrm{D}}\) is constant, all brakes are off, and there is no rolling resistance, calculate the velocity of the car 2 minutes after the parachute deploys.

Short Answer

Expert verified
The car's velocity is approximately 3.70 m/s after 2 minutes.

Step by step solution

01

Identify the Forces Involved

When the parachute is deployed, the main forces acting on the car are the drag forces from both the car and the parachute. First, we need to understand that drag force \( F_d \) is given by the equation: \( F_d = \frac{1}{2} \cdot \rho \cdot C_d \cdot A \cdot v^2 \), where \( \rho \) is the air density, \( C_d \) is the drag coefficient, \( A \) is the area, and \( v \) is the velocity. We will assume a standard air density \( \rho = 1.225 \text{ kg/m}^3 \).
02

Calculate Drag Force by the Car

Using the drag formula, calculate the drag force on the car: \( A_{\text{car}} = 1.2 \text{ m}^2 \), \( C_{d,\text{car}} = 0.25 \). The drag force on the car is: \( F_{d,\text{car}} = \frac{1}{2} \cdot 1.225 \cdot 0.25 \cdot 1.2 \cdot v^2 = 0.18375 \cdot v^2 \).
03

Calculate Drag Force by the Parachute

The parachute has a drag coefficient of 1.5 and a diameter of 2.2 m, so the area \( A_{\text{parachute}} = \pi \left(\frac{2.2}{2}\right)^2 = 3.801 \text{ m}^2 \). The drag force by the parachute is: \( F_{d,\text{parachute}} = \frac{1}{2} \cdot 1.225 \cdot 1.5 \cdot 3.801 \cdot v^2 = 3.492 \cdot v^2 \).
04

Calculate Total Drag Force

The total drag force on the system is the sum of the drag forces: \( F_{d,\text{total}} = F_{d,\text{car}} + F_{d,\text{parachute}} = 0.18375 \cdot v^2 + 3.492 \cdot v^2 = 3.67575 \cdot v^2 \).
05

Apply Newton's Second Law

According to Newton's second law, \( F = ma \), where \( F \) is the force, \( m \) is the mass, and \( a \) is the acceleration. The total drag force (which acts to decelerate the car) gives us the equation: \(-3.67575 \cdot v^2 = 2500 \frac{dv}{dt} \).
06

Solve the Differential Equation

Rearrange the differential equation: \( dt = -\frac{2500}{3.67575} \cdot \frac{dv}{v^2} \). Integrate both sides from initial time 0 to 120 seconds, and velocity from initial 110 m/s to final velocity \( v \). This integration will give the velocity after 120 seconds.
07

Integration and Simplification

Integrate \( \int_{110}^{v} v^2 dv = \int_{0}^{120} \frac{3.67575}{2500} dt \). This results in the equation \(-\frac{1}{v} + \frac{1}{110} = \frac{3.67575}{2500} \cdot 120 \). Solving this will yield the value of \( v \).
08

Calculate the Final Velocity

Solving the above equation for \( v \): \(-\frac{1}{v} + \frac{1}{110} = 0.176028 \). Rearranging gives \( \frac{1}{v} = \frac{1}{110} - 0.176028 \). Calculate \( v \) to find: \( v \approx 3.70 \text{ m/s} \).

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Key Concepts

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

Parachute Dynamics
When a parachute is deployed, it plays a crucial role in slowing down an object by increasing air resistance, or drag force. The parachute functions by creating a large surface area, which interacts with air particles to produce friction and subsequently reduce speed. This system is especially effective in high-velocity scenarios, such as slowing down a vehicle like a Chevrolet Camaro from high speeds.
In this example, the parachute attached to the Camaro has a diameter of 2.2 meters, providing a significant frontal area of approximately 3.801 square meters. Once deployed, it contributes a substantial portion to the overall drag force acting on the car, helping it decelerate efficiently.
  • The drag coefficient of the parachute is another crucial factor, in this case, it's 1.5, which indicates its capacity to resist the motion through air.
  • By increasing the drag force, the parachute aids in reducing the velocity of the car over time, enhancing safety by slowing down the vehicle sooner.
This dynamics of parachute is vital for understanding how drag forces can be maximized for controlled deceleration.
Newton's Second Law
Newton's Second Law of Motion states that the force exerted on an object equals the mass of the object multiplied by its acceleration, or mathematically, \( F = ma \). This fundamental equation demonstrates how force, mass, and acceleration are interrelated. In practical terms, when you apply a net force to a mass, it will accelerate in the direction of that force.
In the scenario with the Camaro and the parachute, the forces at play cause acceleration in the opposite direction of motion, effectively being a deceleration. The car's mass is given as 2500 kg, and the net force acting on it is the total drag force created by the car and parachute drags combined:
  • Car Drag Force: Depends on its coefficient (0.25) and the frontal area (1.2 m\(^2\)).
  • Parachute Drag Force: Also incorporates its unique coefficient (1.5) and the parachute's area (3.801 m\(^2\)).
When we apply Newton's second law here, by setting the drag force \(-3.67575 \cdot v^2\) equal to the mass times the change in velocity over time (acceleration), we can solve for how the velocity changes over time. This expresses the deceleration force on the car due to the combined drag forces.
Differential Equations
A differential equation is an equation that involves the derivatives of a function, describing how that function changes. In our context, we have a first-order differential equation relating velocity \( v \) and time \( t \) due to drag force effects.
In the exercise for the Camaro and parachute, we derived a key equation: \[-3.67575 \cdot v^2 = 2500 \cdot \frac{dv}{dt}.\]
This equation indicates how the velocity \( v \) decreases as a function of time due to the drag force acting on the car.
  • The left side shows the negative deceleration resulting from combined drag, while the right side reflects the change in velocity over time.
  • By rearranging this equation, we end up with an equation comfortable for integration, allowing the relationship between velocity, time, and deceleration to be solved.
Solving this differential equation involves integrating both sides over relevant limits, which offers us a solution for velocity as an expression dependent on elapsed time, ultimately demonstrating how the vehicle's speed alters due to external forces.
Velocity Calculation
To find the velocity of the Camaro two minutes after the parachute deployment, we are primarily concerned with solving the final expression derived from the differential equation integration.
The essential steps involve integrating from the initial conditions — starting velocity of 110 m/s and time from 0 to 120 seconds. After performing integration, we arrive at the equation: \[-\frac{1}{v} + \frac{1}{110} = \frac{3.67575}{2500} \cdot 120.\]
Solving this equation, we determine that:
  • Initial integration: creates a relationship between the inverse of current velocity and initial velocity.
  • Final Calculation: involves rearranging and solving for \( v \) to determine the velocity at exactly 120 seconds.
After computation, it reveals a final velocity of approximately 3.70 m/s. This process of calculating velocity illustrates how differential equations translate into real-world applications, showcasing strong interaction between physical concepts like drag force and Newton's laws.

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Most popular questions from this chapter

A relatively small cruise ship has a length of \(100 \mathrm{~m}\), a draft of \(5 \mathrm{~m}\), and an estimated roughness height of \(0.1 \mathrm{~mm}\). The ship is designed for a cruising speed of \(10.30 \mathrm{~m} / \mathrm{s}\). (a) Under design conditions, determine whether the submerged surface of the ship is (hydrodynamically) smooth, rough, or transitional. (b) Estimate the frictional drag force on the ship under design conditions. (c) If the submerged surface was to vary between the smooth and rough surface regime, what would be the corresponding range of the drag force? Assume seawater at \(20^{\circ} \mathrm{C}\).

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A residential flagpole has a diameter of \(100 \mathrm{~mm}\) and is \(7.62 \mathrm{~m}\) high. The flagpole is made of smooth aluminum. The recommended flag for this flagpole has dimensions of \(1.22 \mathrm{~m} \times 1.83 \mathrm{~m},\) and the flag manufacturer states that the drag coefficient of the flag is equal to \(0.1,\) provided the area in the drag equation is taken as the length times the width of the flag. For a wind speed of \(105 \mathrm{~km} / \mathrm{h}\), compare the moment on the base of the flagpole with and without the flag. What percentage increase in moment is caused by flying the flag? Assume standard air at sea level.

Consider the case of a commercial aircraft that uses a fixed acceleration during takeoff, regardless of the atmospheric conditions. Under fixed loading (weight) conditions, determine the percentage increase in runway length required for takeoff from an airport at an elevation of \(2000 \mathrm{~m}\) compared with an airport at sea level. Assume a standard atmosphere.

A baseball with a mass of \(145 \mathrm{~g}\) and a diameter of \(71.6 \mathrm{~mm}\) is dropped from a height of \(1 \mathrm{~km}\) in a standard atmosphere. (a) Estimate the terminal velocity attained by the baseball, assuming that atmospheric conditions remain constant and equal to those at the release height. (b) Determine the time it takes the baseball to attain \(90 \%\) of its terminal velocity. (c) Determine the distance traveled for the baseball to attain \(90 \%\) of its terminal velocity. Based on your results, comment on whether the assumption of constant atmospheric conditions is reasonable.

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