Sound Power
Intensity : Average Rate of energy transfer per unit area
          W                                        p2
      I           W/m   2
                                 W  4 r I  4 r
                                            2         2
                                                        Watt
         4 r 2                                    0 c
                                                 W
      Sound Power Level:           SWL  10log10      dB
                                                 Wref
                                   Reference Power Wref =10-12 Watt
Peak Power output:
Female Voice  0.002W,      Male Voice  0.004W,                      A
Soft whisper  10-9W, An average shout  0.001W Large
Orchestra  10-70W, Large Jet at Takeoff  100,000W
15,000,000 speakers speaking simultaneously generate 1HP
                 Recap
 Sound Measurement Amplitude/Frequency
 Sound Pressure, Intensity, Power, ISL, PSL
                              Radiation from Source
                       Point Source (Monopole)                                     p 2
                                                             W  4 r 2 I  4 r 2      Watt
                                                                                   0 c
  Radiates sound waves equally in all directions (spherical radiation)
  W: is acoustic power output of the source;
         power must be distributed equally over spherical surface area
                              W  1                     W      1
               IL  10 log10      2 
                                             10 log
                              4 r  I ref            4 1012 r 2
                                                    10
                                  W
               IL  10 log10               20 log10 r
                                4 10 12
                         Constant term      Depends on distance
                                                                           Inverse Square Law
                                            from source
When distance doubles (r=2r0) ; 20log 2 + 20log r0 means 6dB difference in the Sound Intensity Level
If the point source is placed on ground,
it radiates over a hemisphere,
the intensity is then doubled and
                   W  1
    IL  10 log10      2 
                   2 r  I ref
                      W
    IL  10 log10              20 log10 r
                    2 10 12
                                     Line Source
 (Long trains, steady stream of traffic, long straight run of pipeline)
If the source is located on ground,
and has acoustic power output of
W per unit length
radiating over half the cylinder
                                       W
Intensity at radius r,              I
                                       r
                            W
             IL  10log10           10log10 r
                           10 12
When distance doubles;   10log 2 + 10log r means 3dB difference in the Sound Intensity Level
             VALIDITY OF POINT SOURCE
In free field condition,
Any source with its characteristic dimension small compared to
the wavelength of the sound generated is considered a point
source
Alternatively a source is considered point source if the receiver is
at large distance away from the source
Some small sources do not radiate sound equally in all directions
Directivity of the source must be taken into account to calculate
level from the source power
                DIRECTIVITY OF SOUND SOURCE
  Sound sources whose dimensions are small compared to the wavelength of
  the sound they are radiating are generally omni-directional;
  otherwise when dimensions are large in comparison, they are directional
        Sound Intensityat an angle  and at distance r from
        a directional source radiating sound p ower W
Q 
       Sound Intensityat distance r from a omni - directional
       source radiating the same sound p ower W
Directivity Factor & Directivity Index
Directivity Factor                    Directivity Index
     I            p2                DI  10 log10 Q                        4r 2 I
Q      2                           thus
                                                                            
     Is   pS                                                                     Q
                                      DI  L p  L pS
Rigid boundaries force an omni-directional source to radiate sound in preferential direction
    EFFECT OF HARD REFLECTING GROUND
Radiated Sound Power of the source can be affected by a
rigid, reflecting planes
Strength and vibrational velocity of the source does not
change but the hard reflecting plane produces double the
pressure and four-fold increase in sound intensity compared to
monopole (point spherical source)
If source is sufficiently above the ground this effect is reduced
                                       I=0
                                       Uniform
                                       sound
                                       energy
                                       density
Free Field Condition   Diffuse Field
MWL Lab, KTH Sweden
  Finding sound power (ISO 3745)
Measurements made in semi-reverberant and free field conditions
are in error of 2dB
Noise Mapping
Noise Contours
Environmental
   Effects
                                                Wind Gradient
                Hot Sunny
                Day
                              Velocity
                              Gradient (-)
                                             Temperature Gradient
                 Cool Night
                                               Wind & Temp effects tend to
                                               cancel out
                                               Increase or decrease of 5-6dB
Environmental Effects
HUMAN PERCEPTION
                              The Human Ear
Outer Ear: Pinna and auditory canal
concentrate pressure on to drum
Middle Ear: Eardrum, Small Bones
connecting eardrum to inner ear
Inner Ear: Filled with liquid, cochlea
with basilar membrane respond to
stimulus of eardrum with the help of
thousands of tiny, highly sensitive hair
cells, different portions responding
different frequencies of sound.
The movement of hair cells is
conveyed as sensation of sound to the
brain through nerve impulses
Masking takes place at the membrane;
Higher frequencies are masked by
lower ones, degree depends on
freq.difference and relative
magnitudes of the two sounds
                           SOUND BITS
Unless there is a 3 dB difference in SPL, human beings can
not distinguish the difference in the sound
Sound is perceived as doubled in its loudness when there is
10dB difference in the SPL.
(Remember 6dB change represents doubling of sound pressure!!)
Ear is not equally sensitive at all frequencies:
highly sensitive at frequencies between 2kHz to 5kHz
less at other freq.
This sensitivity dependence on frequency is also dependent
on SPL!!!!
            RESPONSE OF HUMAN EAR
                                               Loudness Level
                                               (Phon)
                                               Equal to numerical
                                               value of SPL at
                                               1000Hz
                                               0Phon: threshold of
                                               hearing
                                               Loudness Level
                                               (Phon) useful for
                                               comparing two
                                               different frequencies
                                               for equal loudness
                                               But, 60Phon is still
                                               not twice as loud as
                                               30Phon
                                               Doubling of loudness
                                               corresponds to increase
Equal Loudness Contours for pure tones, Free   of 10Phon
Field conditions
                      Weighting Characteristics
A-weighting: 40Phon equal loudness level contour
C-weighting: 90Phon equal loudness level contour
D-weighting for Aircraft Noise
BASIC SOUND LEVEL METER
LOUDNESS INDEX
          Direct relationship between
          Loudness Level P (Phons) and
          Loudness Index S (Sones)
                        P  40
                 S 2    10
          8 Sones is twice as loud as
          4 Sones
     Hearing Damage Potential to sound energy
     depends on its             level & duration of exposure
 Equivalent Continuous Sound Level (Leq)
                                          tj : Fraction of total time
                                          duration for which SPL of                              
                        Lj                           
                        10 
                  N
                                          Lj was measured
Leq  10 Log10  t j 10  dB
                j 1                          
                                         Total time interval
                                          considered is divided in N
                                          parts
                                          with each part has constant
                                          SPL of Lj
                1 100 7 70                            
Leq  10 Log10  10  10   91dB
                   10    10
               8      8    
Integrating Sound Level Meter for randomly varying sound
e.g., 60sec Leq
Sound Exposure Level (SEL)
Constant level acting for 1sec
that has the same acoustic
energy as the original sound
 Vehicle passing by;
 Aircraft flying over
Noise Dose Meters display
Noise Exposure Measurements
Regulations:
Basis of 90dB(A) for 8hr a day.
ISO(1999): Increase in SPL
from 90 to 93dB(A) must
reduce time of exposure from 8
to 4 hours
OSHA: with every 5dB(A)
increase, reduce exposure by
half
 Occupational Safety and Health Administration
Noise Rating Curves (ISO R 1996)
                                   Level of
                                   Noise
                                   Annoyance
                                    NR78
Errors of the order of 6dB around 400Hz due to reflections
Sources:
Vibration and Noise for Engineers, K Pujara
Fundamentals of Acoustics, Kinsler and Frey
Fundamentals of Noise and Vibration Analysis for
Engineers, M Norton and D Karczub
Introduction to Acoustics, R D Ford
Measuring Sound, B&K Application Notes
Sound Intensity, B&K Application Notes
Basic Concepts of Sound, B&K Application Notes
TRANSFORMER NOISE CASE STUDY
                        SOURCES
The primary source of acoustic noise generation in a transformer is the
periodic mechanical deformation of the transformer core under the
influence of fluctuating electromagnetic flux associated with these parts.
The physical phenomena associated with this tonal noise generation can be
classified as follows:
                                      core laminations strike against each
      vibration of the core           other due to residual gaps between
                                      laminations