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An experimental engine weighing 480 lb is mounted on a test stand with spring mounts at \(A\) and \(B,\) each with a stiffness of 600 lb/in. The radius of gyration of the engine about its mass center \(G\) is 4.60 in. With the motor not running, calculate the natural frequency \(\left(f_{n}\right)_{y}\) of vertical vibration and \(\left(f_{n}\right)_{\theta}\) of rotation about \(G .\) If vertical motion is suppressed and a light rotational imbalance occurs, at what speed \(N\) should the engine not be run?

Short Answer

Expert verified
The natural vertical frequency is 1.43 Hz, rotation frequency 4.45 Hz, and critical speed 267 RPM.

Step by step solution

01

Calculate the Natural Frequency of Vertical Vibration

The natural frequency of vertical vibration is given by the formula:\[(f_n)_y = \frac{1}{2\pi} \sqrt{\frac{k_{total}}{m}}\]where \(k_{total}\) is the total stiffness and \(m\) is the mass of the engine. Each spring mount provides a stiffness of 600 lb/in, so the total stiffness is \(k_{total} = 600 \times 2 = 1200\) lb/in. The engine weight is 480 lb, so the mass \(m\) is calculated by dividing the weight by the gravitational acceleration (32.2 ft/s²), converting \(m = \frac{480}{32.2} \approx 14.9\) slug. Thus,\[(f_n)_y = \frac{1}{2\pi} \sqrt{\frac{1200}{14.9}} \approx 1.43\, \text{Hz}\]
02

Calculate the Natural Frequency of Rotation About G

The natural frequency of rotation about G can be calculated using:\[(f_n)_\theta = \frac{1}{2\pi} \sqrt{\frac{k \cdot r_g^2}{I_g}}\]where \(I_g = m \cdot r_g^2\) is the moment of inertia about G. The given radius of gyration \(r_g\) is 4.60 in, or 4.60/12 ft (converting to feet), so \(I_g = 14.9 \cdot (4.60/12)^2 \approx 2.34\, \text{slug}\cdot\text{ft}^2\). Substitute the values:\[(f_n)_\theta = \frac{1}{2\pi} \sqrt{\frac{600 \cdot (4.60/12)^2}{2.34}} \approx 4.45\, \text{Hz}\]
03

Determine Critical Rotational Speed for Imbalance

The engine should not be operated at the rotational speed that matches its natural frequency, due to the risk of resonance. Therefore, the critical speed \(N\) is the frequency of rotation about the center of mass \((f_n)_\theta\) converted into revolutions per minute. Convert 4.45 Hz to rotations per minute (RPM):\[N = 4.45 \times 60 \approx 267\, \text{RPM}\]

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Key Concepts

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

Vertical Vibration
Vertical vibration refers to the up and down movement of an object due to external forces acting on it. In the context of the experimental engine mounted on springs, the natural frequency of vertical vibration \(f_n\)_y helps us understand how the engine bounces vertically.
  • The natural frequency is crucial because it indicates the rate at which the engine will naturally oscillate when disturbed.
  • A high frequency means faster oscillations, while a low frequency reflects slower bounces.
To calculate this for our engine, which weighs 480 pounds, we must first determine its mass. This involves dividing its weight by the gravitational constant, giving us a mass of around 14.9 slugs.
The total stiffness of the springs (600 lb/in each) is summed to give 1200 lb/in, allowing us to compute the vibrational frequency using the formula:
\[ \(f_n\)_y = \frac{1}{2\pi} \sqrt{\frac{k_{total}}{m}} \]
This calculation results in a natural frequency of approximately 1.43 Hz, meaning the engine will naturally oscillate vertically at this rate.
Rotational Dynamics
Understanding rotational dynamics involves studying how objects rotate and the forces that affect this rotation. When considering the engine's rotation around its center of mass \(G\), we need to compute its natural frequency of rotation \(f_n\)_\theta.
  • Rotational dynamics tells us how the engine will respond to forces causing it to spin or rotate.
  • This is particularly important to predict and avoid resonance, which can occur if the engine's operating frequency matches its natural frequency.
For rotation about its center of mass, the engine’s rotational natural frequency is derived using the formula:
\[ \(f_n\)_\theta = \frac{1}{2\pi} \sqrt{\frac{k \cdot r_g^2}{I_g}} \]
Where the term \(I_g\) represents the engine's moment of inertia, influencing how it rotates.
Moment of Inertia
The moment of inertia \(I_g\) is a critical factor in rotational dynamics. It measures how much torque is needed for a desired angular acceleration around a pivot point. For our engine, this is about its center of mass \(G\).
  • The moment of inertia depends on both the mass of the engine and how that mass is distributed with respect to the axis of rotation.
  • It is often given by the formula: \(I_g = m \times r_g^2\), where \(r_g\) is the radius of gyration.
With a mass \(m\) of 14.9 slugs and a radius of gyration \(r_g\) of 4.60 inches (converted to feet), the engine’s moment of inertia is calculated to be about 2.34 slug\cdot ft².
This value is crucial when predicting how the engine will behave under rotational forces. A higher moment of inertia means that more energy is required to alter its angular velocity.
Radius of Gyration
The radius of gyration \(r_g\) offers a way to understand how the mass of an object is distributed relative to its axis of rotation. For our engine, this value is 4.60 inches about its mass center \(G\).
  • The radius of gyration helps to simplify calculations involving rotational dynamics by acting as a single distance from the axis where the entire mass could be assumed to be concentrated for the same moment of inertia.
  • This simplification is critical in engineering and physics for analyzing rotational motion.
By converting the radius of gyration into feet and using it in our calculations, we align it correctly with the units of stiffness and inertia to predict the engine’s behavior accurately during rotation.
Understanding the radius of gyration allows engineers to design systems that optimize the distribution of mass and therefore control the dynamic behavior of the engine.

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Most popular questions from this chapter

The seismic instrument shown is secured to a ship's deck near the stern where propeller-induced vibration is most pronounced. The ship has a single three-bladed propeller which turns at 180 rev/ \(\min\) and operates partly out of water, thus causing a shock as each blade breaks the surface. The damping ratio of the instrument is \(\zeta=0.5,\) and its undamped natural frequency is \(3 \mathrm{Hz}\). If the measured amplitude of \(A\) relative to its frame is \(0.75 \mathrm{mm},\) compute the amplitude \(\delta_{0}\) of the vertical vibration of the deck.

The uniform solid cylinder of mass \(m\) and radius \(r\) rolls without slipping during its oscillation on the circular surface of radius \(R .\) If the motion is confined to small amplitudes \(\theta=\theta_{0},\) determine the period \(\tau\) of the oscillations. Also determine the angular velocity \(\omega\) of the cylinder as it crosses the vertical centerline. (Caution: Do not confuse \(\omega\) with \(\dot{\theta}\) or with \(\omega_{n}\) as used in the defining equations. Note also that \(\theta\) is not the angular displacement of the cylinder.)

The seismic instrument shown is attached to a structure which has a horizontal harmonic vibration at \(3 \mathrm{Hz}\). The instrument has a mass \(m=0.5 \mathrm{kg},\) a spring stiffness \(k=20 \mathrm{N} / \mathrm{m},\) and a viscous damping coefficient \(c=3 \mathrm{N} \cdot \mathrm{s} / \mathrm{m} .\) If the maximum recorded value of \(x\) in its steady-state motion is \(X=2 \mathrm{mm}\) determine the amplitude \(b\) of the horizontal movement \(x_{B}\) of the structure.

During the design of the spring-support system for the 4000 -kg weighing platform, it is decided that the frequency of free vertical vibration in the unloaded condition shall not exceed 3 cycles per second. (a) Determine the maximum acceptable spring constant \(k\) for each of the three identical springs. (b) For this spring constant, what would be the natural frequency \(f_{n}\) of vertical vibration of the platform loaded by the 40 -Mg truck?

The addition of damping to an undamped springmass system causes its period to increase by 25 percent. Determine the damping ratio \(\zeta\)

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