/*! 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 55 A radio-controlled model airplan... [FREE SOLUTION] | 91Ó°ÊÓ

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A radio-controlled model airplane has a momentum given by \(\left[\left(-0.75 \mathrm{kg} \cdot \mathrm{m} / \mathrm{s}^{3}\right) t^{2}+\right.\) \((3.0 \mathrm{kg} \cdot \mathrm{m} / \mathrm{s}) ] \hat{\mathrm{i}}+\left(0.25 \mathrm{kg} \cdot \mathrm{m} / \mathrm{s}^{2}\right) \hat{t}\) What are the \(x-y\) , and z-components of the net force on the airplane?

Short Answer

Expert verified
The force components are \(F_x = -1.5t\), \(F_y = 0.25\), and \(F_z = 0\).

Step by step solution

01

Understand the given momentum expression

The momentum of the airplane is given by \[p(t) = \left[(-0.75 \text{ kg} \cdot \text{m/s}^3)t^2 + 3.0 \text{ kg} \cdot \text{m/s}\right] \hat{\mathrm{i}} + \left(0.25 \text{ kg} \cdot \text{m/s}^2\right)t \hat{\mathrm{j}}.\] This expression shows that the momentum is a function of time and consists of an \(i\)-component and a \(j\)-component. No \(k\)-component (z-component) is given, so the momentum in the \(z\)-direction is zero.
02

Determine the force components using derivatives

Since force is the time derivative of momentum, we need to differentiate each component of the momentum with respect to time to find the corresponding force components. The general relationship is \[F(t) = \frac{d}{dt}[p(t)].\]
03

Differentiate the \(x\)-component of momentum

The \(x\)-component of momentum is \[p_x(t) = (-0.75 \text{ kg} \cdot \text{m/s}^3)t^2 + 3.0 \text{ kg} \cdot \text{m/s}.\] Differentiating this with respect to \(t\), we get \[F_x(t) = \frac{d}{dt}[(-0.75)t^2 + 3.0] = -1.5t \text{ kg} \cdot \text{m/s}^2.\]
04

Differentiate the \(y\)-component of momentum

The \(y\)-component of momentum is \[p_y(t) = (0.25 \text{ kg} \cdot \text{m/s}^2)t.\] Differentiating this with respect to \(t\), we get \[F_y(t) = \frac{d}{dt}[(0.25)t] = 0.25 \text{ kg} \cdot \text{m/s}^2.\] This term is constant, indicating constant force in the Y-direction.
05

Identify the \(z\)-component of momentum

There is no \(z\)-component \((k\)-component) in the momentum expression given. Therefore, the momentum in the \(z\)-direction is zero, and hence the force in the \(z\)-direction is also zero, i.e., \[ F_z = 0. \]

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Key Concepts

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

Time Derivative
In physics, the time derivative of a quantity is a way to describe how that quantity changes as time progresses. In the context of momentum, which describes the motion of an object, the time derivative of momentum gives us the force acting on that object. This is because force is defined as the rate of change of momentum with respect to time.

For example, if you have a momentum function in terms of time, such as \( p(t) \), to find the force \( F(t) \), you take the derivative of \( p(t) \) with respect to \( t \). This operation gives you the expression for force at any time \( t \).

In our exercise, the momentum of the airplane is given by
\[ p(t) = [(-0.75 \ \text{kg} \cdot \text{m/s}^3)t^2 + 3.0 \ \text{kg} \cdot \text{m/s}] \hat{\mathrm{i}} + [0.25 \ \text{kg} \cdot \text{m/s}^2)t \hat{\mathrm{j}}. \]
Taking the time derivative of each component helps determine the force in each direction.
Force Components
When breaking down forces, it's important to understand which direction each component is acting. The forces in physics are vector quantities, which means they have both magnitude and direction. The components of a force vector allow us to analyze how the force affects motion in different directional axes - typically denoted as \( x \), \( y \), and \( z \).

In the provided momentum equation, there are components along the \( x \)-axis (i-component) and \( y \)-axis (j-component), but not the \( z \)-axis (k-component).
  • The \( x \)-component of momentum is given as \( (-0.75 \ \text{kg} \cdot \text{m/s}^3)t^2 + 3.0 \ \text{kg} \cdot \text{m/s} \). When you differentiate it with respect to time, you derive the x-component of force: \( F_x(t) = -1.5t \ \text{kg} \cdot \text{m/s}^2 \).
  • The \( y \)-component of momentum is \( (0.25 \ \text{kg} \cdot \text{m/s}^2)t \), which, when differentiated with respect to time, gives a constant \( y \)-component of force: \( F_y(t) = 0.25 \ \text{kg} \cdot \text{m/s}^2 \).
Recognizing these components is key to determining how forces are at play in various directions.
Radio-Controlled Model
In exercises involving a radio-controlled model, like in this scenario, it is useful to visualize the model as a small-scale airplane that you can pilot remotely. These models are popular in aerodynamics studies as well as hobbies.

When analyzing such models, you often consider various forces and motions associated with them:
  • They have engines that provide thrust, leading to a momentum change over time.
  • Factors like air resistance and gravity also impact the forces acting on them.
  • Understanding the derivatives of momentum gives insight into the dynamics and control of these models.
For our problem, while we do not delve into specific aerodynamic forces, the exercise helps grasp the basics of motion and forces that can apply to radio-controlled aircraft. These models can serve as educational tools for understanding larger, more complex systems in aerodynamics.

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