/*! 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 87 The thin circular disk of mass \... [FREE SOLUTION] | 91Ó°ÊÓ

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The thin circular disk of mass \(m\) and radius \(R\) is hinged about its horizontal tangent axis to the end of a shaft rotating about its vertical axis with an angular velocity \(\omega .\) Determine the steady-state angle \(\beta\) assumed by the plane of the disk with the vertical axis. Observe any limitation on \(\omega\) to ensure that \(\beta>0\)

Short Answer

Expert verified
The steady-state angle \( \beta \) is determined by \( \tan(\beta) = \frac{\omega^2 R}{2g} \). The limitation is \( \omega > 0 \).

Step by step solution

01

Analyze the Forces and Torques Acting on the Disk

The disk is subject to two main forces: the gravitational force, which acts downward through its center of gravity, and the centrifugal force, which acts horizontally due to the rotation about the vertical axis. To find the steady-state angle \( \beta \), these forces must create equal torques about the hinge axis.
02

Determine the Torque from Gravitational Force

The gravitational force creates a torque \( \tau_g = mg \frac{R}{2} \sin(\beta) \) about the hinge, where \( m \) is the mass of the disk, \( g \) is the gravitational acceleration, and \( \frac{R}{2} \) is the distance from the hinge to the center of mass of the disk.
03

Calculate the Torque from Centrifugal Force

The centrifugal force has magnitude \( F_c = m \omega^2 \frac{R}{2} \sin(\beta) \), directed outward horizontally. This force creates a torque \( \tau_c = m \omega^2 \frac{R}{2}^2 \cos(\beta) \) about the hinge.
04

Establish the Equilibrium Condition

For equilibrium and to find the steady-state angle \( \beta \), set the torques equal: \[ mg \frac{R}{2} \sin(\beta) = m \omega^2 \frac{R^2}{4} \cos(\beta) \]Simplifying, we find: \[ g \sin(\beta) = \frac{\omega^2 R}{2} \cos(\beta) \]
05

Solve for \( \tan(\beta) \)

Divide both sides by \( \cos(\beta) \) to obtain:\[ \tan(\beta) = \frac{\omega^2 R}{2g} \]
06

Evaluate the Condition for \( \beta > 0 \)

To ensure \( \beta > 0 \), \( \tan(\beta) \) must be positive, which it is as long as \( \omega^2 R > 0 \). The only limitation is that \( \omega \) must not be zero.

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Key Concepts

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

Gravitational Force
Gravitational force is a fundamental concept in physics, representing the attraction between masses. In the scenario with the circular disk, gravitational force acts vertically downward through the center of gravity of the disk. This force is crucial in determining the torque it produces about the hinge axis. With magnitude calculated as \( F_g = mg \), where \( m \) is the mass of the disk and \( g \) is the acceleration due to gravity, it plays a vital role in the rotational dynamics of the disk.

In the evaluated exercise, gravitational force contributes to the torque\( \tau_g \). The torque from this force is determined by the perpendicular distance from the axis of rotation to the line of action of the force, resulting in the expression \( \tau_g = mg \frac{R}{2} \sin(\beta) \). Understanding this relationship helps us evaluate the disk's behavior under different rotational conditions.
Centrifugal Force
Centrifugal force is often thought of as an 'apparent' force felt by an object moving in a circular path. As the disk rotates around the vertical axis with angular velocity \( \omega \), centrifugal force acts outward, perpendicular to the axis of rotation.

In our problem, it is vital to consider this force to predict the disk's steady-state angle. The magnitude of centrifugal force is \( F_c = m \omega^2 \frac{R}{2} \sin(\beta) \), and it induces a torque \( \tau_c \) around the hinge. This torque due to the centrifugal force is formulated as \( \tau_c = m \omega^2 \frac{R^2}{4} \cos(\beta) \). This concept ensures a balanced equation of motion when combined with gravitational torque, helping us solve for the angle \( \beta \).
Steady-State Equilibrium
Achieving steady-state equilibrium requires that the torques acting on the disk balance each other. This balance means the torques from gravitational force \( (\tau_g) \) and centrifugal force \( (\tau_c) \) must be equal.

For the thin disk in question, equilibrium is reached when \( mg \frac{R}{2} \sin(\beta) = m \omega^2 \frac{R^2}{4} \cos(\beta) \). Simplifying this relationship leads us to the expression \( \tan(\beta) = \frac{\omega^2 R}{2g} \), guiding us to determine \( \beta \).

This condition implies that the plane of the disk will stabilize at an angle \( \beta \), where neither gravitational nor centrifugal forces dominate, allowing for a constant, unchanging motion in the system.
Torque Analysis
Torque analysis is pivotal in understanding rotational motion. Torque is the measure of the force causing an object to rotate about an axis. In our exercise, torque arises from both gravitational and centrifugal forces.

The formula for gravitational torque \( \tau_g \) is \( mg \frac{R}{2} \sin(\beta) \) and for centrifugal torque \( \tau_c \) is \( m \omega^2 \frac{R^2}{4} \cos(\beta) \). Comparing these allows us to set an equilibrium condition where both torques are equal.

Solving this gives us insights into how rotational speed \( (\omega) \) affects the disk position and highlights the role of torque in maintaining system stability.
Angular Velocity
Angular velocity \( \omega \) indicates the rate of rotation about an axis. It plays a significant role in analyzing rotational dynamics, especially in our disk example.

Higher angular velocities increase the centrifugal force, noticeably affecting the torque balance necessary for steady-state equilibrium. The relationship \( \tan(\beta) = \frac{\omega^2 R}{2g} \) illustrates how angular velocity can shift the steady-state angle \( \beta \).

For \( \beta > 0 \), \( \omega \) must have a non-zero value. Angular velocity doesn't just determine speed; it directly influences force distribution on the disk, serving as a critical factor in rotational dynamics analysis.

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Most popular questions from this chapter

The uniform circular disk of 4 -in. radius and small thickness weighs 8 lb and is spinning about its \(y^{\prime}\) axis at the rate \(N=300\) rev/min with its plane of rotation tilted at a constant angle \(\beta=20^{\circ}\) from the vertical \(x-z\) plane. Simultaneously, the assembly rotates about the fixed \(z\) -axis at the rate \(p=60\) rev/min. Calculate the angular momentum \(\mathbf{H}_{O}\) of the disk alone about the origin \(O\) of the \(x-y-z\) coordinates. Also calculate the kinetic energy \(T\) of the disk.

Each of the slender rods of length \(l\) and mass \(m\) is welded to the circular disk which rotates about the vertical \(z\) -axis with an angular velocity \(\omega .\) Each rod makes an angle \(\beta\) with the vertical and lies in a plane parallel to the \(y-z\) plane. Determine an expression for the angular momentum \(\mathbf{H}_{O}\) of the two rods about the origin \(O\) of the axes.

The helicopter is nosing over at the constant rate \(q\) rad/s. If the rotor blades revolve at the constant speed \(p\) rad/s, write the expression for the angular acceleration \(\alpha\) of the rotor. Take the \(y\) -axis to be attached to the fuselage and pointing forward perpendicular to the rotor axis.

An experimental car is equipped with a gyro stabilizer to counteract completely the tendency of the car to tip when rounding a curve (no change in normal force between tires and road). The rotor of the gyro has a mass \(m_{0}\) and a radius of gyration \(k\) and is mounted in fixed bearings on a shaft which is parallel to the rear axle of the car. The center of mass of the car is a distance \(h\) above the road, and the car is rounding an unbanked level turn at a speed \(v .\) At what speed \(p\) should the rotor turn and in what direction to counteract completely the tendency of the car to overturn for either a right or a left turn? The combined mass of car and rotor is \(m\)

The blades and hub of the helicopter rotor weigh 140 lb and have a radius of gyration of \(10 \mathrm{ft}\) about the \(z\) -axis of rotation. With the rotor turning at 500 rev/min during a short interval following vertical liftoff, the helicopter tilts forward at the rate \(\dot{\theta}=10\) deg/sec in order to acquire forward velocity. Determine the gyroscopic moment \(M\) transmitted to the body of the helicopter by its rotor and indicate whether the helicopter tends to deflect clockwise or counterclockwise, as viewed by a passenger facing forward.

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