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List of Symbols

Dynamic Performance Investigation of Base Isolated Structures
By Ather K. Sharif
Definition of decibel scaling used

It is important that the signal of interest, in this case the response due to the train source is clearly above ambient levels

The magnitude of a level in decibels is ten times the logarithm to the base 10 of the ratio of power-like quantities, i.e.


where: L level of power-like quantity

= quantity under consideration

XO = reference quantity of the same kind

A difference in the levels of two like quantities X1 and X2 is described by the same formula because, by the rules of logarithms, the reference quantity is automatically divided out as follows:

Where Transmissibility (insertion loss or gain) is defined as the non-dimensional ratio of the response amplitude of a system to the excitation amplitude. The ratio may be one of forces, displacements, velocities or accelerations. A doubling of level causes a 6dB increase, and a tenfold change is equivalent to 20dB. positive insertion loss indicates a disbenefit, and conversely a negative insertion loss indicates a benefit.

The word ‘disbenefit’ is not currently in the English dictionary, although is used to convey the obvious interpretation.

Abbreviations used in Figures

SDOF single degree of freedom

FE finite element


Trans transmissibility


crit critical damping ratio


ch channel


psd power spectral density (auto spectrum)


col column


TR test room


V vertical


L longitudinal


T tangential

List of Symbols
Chapter 2

h depth of source


VP P wave velocity


VR Rayleigh wave velocity


VS S wave velocity

Chapter 3

aw frequency weighted acceleration

t time


VDV Vibration Dose Value

Chapter 5

(t) function of time

fS spring force


fD damping force

 

fI inertial force

 

k spring constant

 

c damping coefficient

 

cc critical damping coefficient

 

m mass

 

p, po applied force

 

u displacement

 

ù du/dt (velocity)

 

ü d2u/dt2 (acceleration)

 

ur relative displacement

 

U absolute displacement

 

ug ugo ground displacement

 

peff effective load

 

Z arbitrary complex constant

 

s constant

 

w n undamped natural angular frequency

 

w D damped natural angular frequency

 

x damping ratio

 

Z1, Z2 constants

 

A constant

 

B constant

 

C vector amplitude

  • vector amplitude

q phase angle

 

G1 G2 constants

  • frequency ratio
  • phase angle

y 1, y 2 phase angles

 

M Dynamic magnification factor

 

W work over cycle

 

t time

 

T transmissibility

 

h , h o loss factor

 

fn natural cyclic frequency

 

j mode number

 

w j angular frequency of mode j

 

L length of column

 

m integer

 

E Young’s modulus

  • density

 

x j modal critical damping ratio

 

w j angular frequency of mode j

 

D w j frequency interval for mode j

  • alpha, Rayleigh damping constant
  • beta, Rayleigh damping constant

d m logarithmic decrement determined from waveform m cycles apart

 

w frequency point above resonance

 

w frequency point below resonance

 

w resonance frequency

 

q a angle to point (a) above resonance

 

q b angle to point (b) below resonance

 

K constant

 

 -1

 

Re real

 

Im imaginary

Chapter 6

Gxx auto spectra of stationary random process x(t)

 

Gyy auto spectra of stationary random process y(t)

 

Gxy cross spectra between two stationary random processes

 

x(t) and y(t)

 

Ttotal Total transmissibility

 

Tdirect Direct transmissibility

 

x(t) function of time (t)

 

y(t) function of time (t)

 

h(t ) unit impulse response function

 

H(f) Fourier transform of impulse response function

 

Y(f) finite Fourier transform of y(t)

 

X(f) finite Fourier transform of x(t)

 

g xy2(f) coherence function

  • standard deviation

mean value of a random variable

 

Be effective bandwidth of spectral window

 

T record length

  • number of statistical degrees of freedom

n number of adjacent spectral lines to the side of central value

 

e b bias error

 

Br half power point bandwidth at resonance

 

x critical damping ratio

 

fr resonance frequency

 

e r random error

 

To optimum averaging time

 

Bo optimum bandwidth

 

CT time resolution bias error coefficient

Chapter 7

Transmissibilities

 

D1 test block to un-loaded raft

 

D2 test block to raft loaded with un-isolated mass on ‘rigid’ blocks

 

D3 test block to un-isolated mass

 

D4 test block to isolated mass

 

D5 test block to raft loaded with isolated mass

 

D6 raft loaded with isolated mass to isolated mass

 

S= Component area

 

a i = Component sound absorption coefficient

 

W = sound power (watts)

 

r c = characteristics impedance of air (407 mks rayls)

 

Sx = area of radiating surface (m2)

 

V = r.m.s velocity of vibration of surface (m/s)?

 

SWL = Sound Power Level (dB) ?

 

Wref = 10-12 watts

 

SPL =Sound Pressure Level (dB re20m Pa)?

 

 

S = total surface area of room (m2)

 

Lp = SPL dB re 20Pa

 

La = rms vibration acceleration of floor (re: 10-6g)

 

f = frequency, either octave or 1/3rd octave

 

Lv = Vibration re 10-5m/s2

 

LAmaxf = A-weighted maximum SPL using fast time weighting

 

Lvmax = vibration velocity re 10-9 m/sec

Chapter 10
Appendix 3.1

aw frequency weighted acceleration

 

VDV Vibration Dose Value

 

eVDV estimated Vibration Dose Value

 

aw(rms) r.m.s frequency weighted acceleration

 

t event duration

 

n event number

 

N total number of events

 

r.m.s root mean square

 

r.m.q root mean quad

Appendix 8.1

F = force

 

mr = mass x radius of gyration

 

w = angular frequency

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