Homework 4 Me 3323 Mechanical Vibrations Summer 2015 Utsa As

1hw 4me 3323 Mechanical Vibrations Summer 2015 Utsaassigned 0707

Analyze the assignment question: The task involves solving multiple problems related to mechanical vibrations, probability, and normal distribution concepts. The core requirements include calculating dynamic amplification/attenuation of a single-degree freedom system, finding resonance conditions for a cantilever beam, determining damping coefficients and transmitted forces, analyzing torsional oscillations, deriving responses of vibratory systems, and solving probability problems related to distributions and statistics.

Compute and interpret the dynamic amplification factor of a given mechanical system excited at a specified frequency. Determine the motor speed at which a vibratory response is minimized when subjected to an unbalanced force. Calculate the damping coefficient and dynamic transmitted force of a damped mass-spring system. Analyze torsional oscillations under harmonic excitation. Derive the steady-state response of a torsional system with multiple forcing functions. Formulate the expression of an accelerometer's output in a periodically vibrating system. Additionally, answer detailed probability questions involving normal distributions, binomial probabilities, and related statistical measures.

In essence, the assignment encompasses solving physical vibration systems' response parameters, understanding damping and resonance phenomena, and applying probability theory to real-world data distributions.

Sample Paper For Above instruction

Introduction

Mechanical vibrations are fundamental in understanding dynamic response characteristics of engineering systems. Analyzing how structures such as beams and mass-spring-damper setups respond under harmonic excitation provides insights critical for designing resilient systems. Concurrently, probability theory underpins the statistical modeling necessary to interpret variability in real-world data, such as manufacturing tolerances or experimental measurements. This paper explores various aspects of vibratory response calculation, damping estimation, resonance avoidance, and probabilistic analysis, integrating theoretical foundations with practical applications.

Part 1: Dynamic Amplification of a Single Degree of Freedom System

The dynamic response of a single-degree-of-freedom (SDOF) system subjected to harmonic excitation is characterized by the amplification factor, defined as the ratio of the steady-state displacement amplitude to the static displacement generated by the same load. Mathematically, this is expressed as:

X / Xstatic = 1 / √[(1 - r2)2 + (2ζr)2]

where r is the frequency ratio (ω / ωn), and ζ is the damping ratio (c / 2mωn). Given the parameters: m = 100 kg, k = 20,000 N/m, c = 6000 Ns/m, and excitation frequency ω = 100 rad/sec, the first step involves calculating ωn:

ωn = √(k/m) = √(20000/100) = √200 ≈ 14.14 rad/sec.

Since the excitation frequency ω = 100 rad/sec, the frequency ratio r ≈ 100 / 14.14 ≈ 7.07. Next, calculate the damping ratio ζ:

ζ = c / (2mωn) = 6000 / (2 100 14.14) ≈ 6000 / 2828 ≈ 2.12.

Because ζ > 1, this reflects an overdamped system with minimal resonance, and the amplification factor reduces significantly. Applying the formula yields:

X / Xstatic ≈ 1 / √[(1 - 7.072)2 + (22.127.07)2] ≈ 1 / √[(1 - 50)2 + (302)] ≈ 1 / √[(−49)2 + 900] ≈ 1 / √(2401 + 900) ≈ 1 / √(3301) ≈ 1 / 57.45 ≈ 0.017.

This indicates significant attenuation at high driving frequencies, aligning with the physical understanding that damping and off-resonance conditions suppress system amplitudes.

Part 2: Resonance Avoidance in a Cantilever Beam

For a cantilever beam with a mounted motor, the deflection under unbalanced force is related to the dynamic response at the beam tip. The maximum response amplitude is given by:

δmax = (Funbal / keff) × Dynamic Amplification Factor (DAF).

When the motor's rotational speed induces a harmonic excitation, the effective frequency is ωm = 2πN/60, where N is rpm. The natural frequency of the beam is derived from its properties, but since mass of the beam is negligible, the effective system behaves like a mass-spring system with negligible mass. To keep the amplitude less than δ0 = 10 mm, the excitation frequency must avoid resonance.

Given that the unbalanced force is 100 N at 1800 rpm, and the deflection is 10 mm, the response at the new speed Nnew can be controlled by tuning N such that the excitation frequency ωm does not approach the system's natural frequency. Thus, Nnew can be calculated by setting the response ratio to less than the specified limit, effectively avoiding resonance.

Part 3: Damped Oscillation Parameters

Given a damped system with mass m = 20 kg, stiffness k = 2400 N/m, and response amplitude of 0.02 m at resonance, the damping coefficient c is determined by the relation between the response amplitudes and the damping ratio ζ:

The amplitude ratio at resonance is:

R = X / X0 = 1 / (2ζ),

Rearranged to find ζ:

ζ = 1 / (2R) = 1 / (2 (0.02 / 0.007)) ≈ 1 / (2 2.86) ≈ 0.175.

Calculating c:

c = 2ζmωn = 2 0.175 20 √(2400/20) ≈ 0.35 20 10.954 ≈ 0.35 219.09 ≈ 76.68 Ns/m.

The dynamic force transmitted to the support is:

Ftransmitted = kX + c(ωn)X, which computes to concrete values once ωn and amplitude are known.

Part 4: Torsional Oscillations and Steady-State Response

The governing differential equation includes mass moment of inertia, damping, stiffness, and harmonic excitation components. The steady-state response can be obtained by solving the differential equation using complex exponential solutions or phasor methods, considering the forcing functions. The detailed calculations involve deriving the particular solutions and calculating amplitude and phase shift based on the excitative frequencies.

Part 5: Accelerometer Response in Periodic Motion

The accelerometer's output response to periodic displacement involves the damping factor ζ, natural frequency ωn, and the excitation motion components. The output acceleration can be expressed as a combination of sinusoidal responses with amplitude modifications due to damping, following the general form:

a(t) = A0 cos(ωt + φ), where A0 depends on the input displacement and system parameters.

Probability and Statistics Analyses

In addition to vibrational analysis, the assignment requires proficiency in probability theory. The questions cover classical probability, normal distribution quantiles, binomial probabilities, and statistical measures like mean and standard deviation. For example, calculating the probability that a random variable exceeds a threshold involves converting the raw score to a Z-score and consulting standard normal distribution tables.

Particularly, calculating the probability of a customer spending more than a certain amount involves standardizing the value and referencing the normal distribution curve. Binomial probabilities are derived from the binomial formula: P(X = k) = C(n, k) pk (1 - p)n - k. These concepts are important in risk assessment, quality control, and decision-making processes.

Conclusion

Understanding system responses in vibratory scenarios requires application of dynamic equations, damping considerations, and resonance avoidance strategies. Probabilistic analysis complements this by modeling uncertainties inherent in real-world systems and measurements. Together, these approaches enhance the design, analysis, and operational safety of mechanical systems.

References

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