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Structures Vibration Frequency

Reference data and engineering information about structures vibration frequency for mechanics applications.

structuresvibrationfrequency

Overview

Engineering reference data for Structures Vibration Frequency in mechanics.

Key Formulas

Newton's Second Law

F=maF = ma

Force = mass × acceleration.

Work

W=FdcosθW = Fd\cos\theta

Work = force × displacement × cos(angle).

Kinetic Energy

Ek=12mv2E_k = \frac{1}{2}mv^2

Energy of motion.

Potential Energy

Ep=mghE_p = mgh

Gravitational potential energy.

Variables

SymbolDescriptionUnit
FFForceN
mmMasskg
aaAccelerationm/s²
vvVelocitym/s

Vibration Assessment Guidelines

  • Vibrations in structures are activated by dynamic periodic forces such as wind, people, traffic, and rotating machinery.
  • For normal floors with a span-to-depth ratio less than 25, vibrations are generally not an issue.
  • For lightweight structures with spans above 8 meters (24 feet), vibrations may occur.
  • As a rule of thumb, the natural frequency of a structure should be greater than 4.5 Hz to ensure it does not compromise strength, stability, or human sensitivity.
  • The numerical factor aa in the general formula for distributed mass is typically taken as 18 for practical accuracy, though it varies between 16 and 20 for similar systems.

Example: Natural Frequency Calculation for a Steel Beam

Consider a simply supported DIN 1025 I 200 steel beam with distributed mass:

  • Length, L=12L = 12 m
  • Moment of Inertia, I=2140×108I = 2140 \times 10^{-8} m4^4
  • Modulus of Elasticity, E=200×109E = 200 \times 10^9 N/m2^2
  • Distributed mass per unit length, q=26.2q = 26.2 kg/m

Using the formula for natural frequency of a simply supported structure with distributed mass: f=π2EIqL4f = \frac{\pi}{2} \sqrt{\frac{E I}{q L^4}}

Substitute the values: f=π2(200×109)(2140×108)(26.2)(12)4f = \frac{\pi}{2} \sqrt{\frac{(200 \times 10^9) (2140 \times 10^{-8})}{(26.2) (12)^4}}

First, compute EIE I: EI=(200×109)×(2140×108)=4.28×106N⋅m2E I = (200 \times 10^9) \times (2140 \times 10^{-8}) = 4.28 \times 10^6 \, \text{N·m}^2

Next, compute qL4q L^4: L4=(12)4=20736m4L^4 = (12)^4 = 20736 \, \text{m}^4 qL4=26.2×20736=543619.2kg⋅m4q L^4 = 26.2 \times 20736 = 543619.2 \, \text{kg·m}^4

Then, the ratio: EIqL4=4.28×106543619.27.87m2\frac{E I}{q L^4} = \frac{4.28 \times 10^6}{543619.2} \approx 7.87 \, \text{m}^{-2}

Square root: 7.872.81m1\sqrt{7.87} \approx 2.81 \, \text{m}^{-1}

Finally, frequency: f=π2×2.811.57×2.81=4.41Hzf = \frac{\pi}{2} \times 2.81 \approx 1.57 \times 2.81 = 4.41 \, \text{Hz}

Since 4.41Hz4.41 \, \text{Hz} is close to the 4.5 Hz threshold, the beam's vibration characteristics should be evaluated carefully for occupancy comfort.

References