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Note: This is a primitive study which is well behind current understanding of this issue, particularly regarding effects on people, but it is important because it is the basis for many current Federal policies regarding aviation noise. It does have a very complete section on definitions.
U.S. DEPARTMENT OF COMMERCE
National Technical Information Service
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Perceived Noise level (PNL) |
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Sound Exposure Level (SEL) |
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24-Hour Above (TA) |
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Day, Evening, Night (TA) |
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Evaluation of the DNL Metric for Heliport/ Helistop Noise Impact Assessment |
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PAGE 10.3
10.4
10.5
10.5.1
10.5.2
10.6
10.7
Section 11.0
11.1
11.2
11.2.1
11.2.2
11.2.3
11.2.4
11.3
Section 12.0
12.1
12.2
12.3
12.4
Section 13.0
13.1
13.2
13.3
13.3.1
13.3.2
Section 14.0
14.1
14.2
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Permissible Distance Between a Speaker and Listeners of Voice and Ambient Level |
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AI |
Articulation Index |
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AICUZ |
Air Installation Compatible Use Zones |
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AIR |
Aerospace Information Report |
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ALM |
A-Weighted Maximum Sound Level |
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ANSI |
American National Standards Institute |
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ARP |
Aerospace Recommended Practice |
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CHABA |
Committee on Hearing, Bioacoustics and Biomechanics |
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CNEL |
Community Noise Equivalent Level |
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CNR |
Composite Noise Rating |
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dB |
Decibel |
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DNL |
Day-Night Average Noise Level |
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DOT |
Department of Transportation |
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DRC |
Damage Risk Criteria |
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EPA |
Environmental Protection Agency |
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EPNL |
Effective Perceived Noise level |
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HUD |
Housing and Urban Development |
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Hz |
Hertz |
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ICAO |
International Civil Aviation 0rganization |
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IEC |
International Electrotechnical Commission |
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ISO |
International Standards 0rganization |
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Ldn |
Day-Night Average Sound Level |
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Leq |
Equivalent Sound Level |
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Lx |
An Airport Cumulative Metric Derived from dBA |
Top NASA National Aeronautics and Space Administration NEF Noise Exposure Forecast NIPTS Noise Induced Permanent Threshold Shift NNI Noise and Number Index NREM Non-Rapid Eye Movement Sleep NTSB National Transportation Safety Board OSHA Occupational Safety and Health Administration PNL Perceived Noise Level PNLT Tone Corrected Perceived Noise Level PSIL Preferred Speech Interference Level REM Rapid Eye Movement Sleep SAE Society of Automotive Engineers SEL Sound Exposure Level SIL Speech Interference Level SST Super Sonic Transport TA Time Above (a certain noise level) TTS Temporary Threshold Shift
Section 1.0 General Introduction
Top
Typical Decibel (dBA) Values Encountered in Daily Life and Industry*
Aviation noise significantly affects
several million people in the United States. In a great number of instances,
aircraft noise simply merges into the urban din, a cacophony of buses, trucks,
motorcycles, automobiles and construction noise. However, in locations closer to
airports and aircraft flight tracks, aircraft noise becomes more of a concern.
The Federal Aviation Administration (FAA) presents this report in an effort to
enhance public understanding of the impact of noise on people and to answer many
questions that typically arise. Information on aircraft noise indices, human
response to noise, and criteria for land use controls is included. Additionally,
information on hearing damage is presented, along with occupational health
standards for noise exposure.
This document has been developed after
reviewing the rather extensive literature in each topical area, including many
original research papers, and also by taking advantage of literature searches
and reviews carried out under FAA and other Federal funding over the past two
decades. Efforts have been made to present the critical findings and conclusions
of pertinent research, providing, when possible, a "bottom line" conclusion,
criterion, or perspective to the reader concerned with aviation
noise.
How to Read This Document
1. If you want only a
general, non-technical presentation of the fundamental issues and concerns with
aircraft noise, read this introduction and the one-page summaries at the
beginning of each section.
2. If you are an engineer, planner, social
scientist or an individual conducting an environmental impact, assessment,
consider reading each section of interest in its entirety.
3. If you wish
to do an in-depth study, assessment or analysis, delve into the text and the
references listed. For more information, consider contacting the staff of the
FAA 0ffice of Environment and Energy, Noise Abatement Division,, in Washington,
D.C. 20591.
What is Sound?
Sound is a complex vibration
transmitted through the air which, upon reaching our ears, may be perceived as
beautiful, desirable, or unwanted. It is this unwanted sound which people
normally refer to as noise.
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Rustling leaves |
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Room in a quiet dwelling at midnight |
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Soft whispers at 5 feet |
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Men's clothing department of large store |
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Window air conditioner |
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Conversational speech |
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Household department of large store |
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Busy restaurant |
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Typing pool (9 typewriters in use) |
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Vacuum cleaner in private residence (at 10 feet) |
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Ringing alarm clock (at 2 feet) |
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Loudly reproduced orchestral music in large room |
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Beginning of hearing damage if prolonged exposure over 85 dBA
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Printing press plant |
86 |
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Heavy city traffic |
92 |
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Heavy diesel-propelled vehicle (about 25 feet away) |
92 |
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Air grinder |
95 |
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Cut-off saw |
97 |
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Home lawn mower |
98 |
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Turbine condenser |
98 |
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150 cubic foot air compressor |
100 |
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Banging of steel plate |
104 |
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Air hammer |
107 |
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Jet airliner (500 feet overhead) |
115 |
* When distances are not specified, sound levels are the value at the
typical location of the machine operator.
Top How Does Sound Get Around? Sound moves outward from its point of origin in waves just as ripples move
outward from the point at which a pebble enters a pond.
While hearing damage is not a common result of aircraft noise exposure,
speech and sleep interferences are major concerns of neighbors close to
airports.
Top Years of experience in airport planning and development have resulted in
guidelines which match uses of land -- like hospitals or concert halls -- with
normally compatible noise levels; these guidelines are published in an FAA
regulation called Federal Aviation Regulation (FAR) PART 150. Implementation of
an FAR150 study will assist airport operators and neighbors in minimizing the
extent of non-compatible land uses.
Top
INTRODUCTION
Top (2) Single Event Energy Dose (3) Cumulative Energy Average Metrics (4) Cumulative Time Metrics
It was originally employed for sounds less than 55 dB in level; now A-level
is used for all levels of sound because it has been found to correlate well with
people's subjective judgment of the loudness of sounds. Its simplicity and
superiority over unweighted SPL in predicting people's responses to noise have
contributed to its wide acceptance. The ALM is currently used for noise
certification of small propeller-driven aircraft; also, in FAA Advisory Circular
36-3C it is used as the basis for airport access restrictions which discriminate
solely on the basis of noise level.
Top
Top acoustical energy associated with the fluctuating sound (during the
prescribed time period) is equal to the total acoustical energy associated with
a steady sound level of Leq for the same period of time. The purpose of Leq is
to provide a single number measure of noise averaged over a specified time
period.
Top 1) Pragmatically speaking, it works. Engineers and planners have acquired
over 30 years working experience with a nominal 10 dB nighttime weighting
function. This experience has been successful, contributing to wise zoning and
planning decisions.
Top
Sound, just as
the ripple in the pond, requires a medium in which to travel; this medium is
usually air.
What is a Decibel?
The decibel (dB) is a
shorthand way to express the amplitude of sound (the relative height of those
ripples in the pond). Because the "ripples" of sound typically experienced may
vary in height from 1 to 100,000 "units", it becomes rather cumbersome to
maintain an intuitive feeling for what different values represent. The decibel
allows people to understand sound strength using numbers ranging between 20 and
120, a more familiar and manageable set of values. Table 1.1 provides a
listing Of some typical sounds and their respective sound levels (expressed in
decibels) at given distances.
The decibel also relates well to the way in
which people perceive sound. A 10 dB increase in a sound seems twice as loud to
the listener, while a 10 dB decrease seems only half as loud. In general,
changes in sound level of 3 or 4 dB are barely perceptible.
What is
Frequency or Pitch?
Some of the ripples in the pond may be very
short; these are analogous to high pitched sounds such as the voice of a
soprano. Other wavelets might be very broad; these waves are analogous to a bass
or baritone voice. Most sounds we hear are composed of a mixture of these
different length sound waves, giving complexity, richness and character to our
experience of sound.
What is the Most Important Effect of Aviation
Noise?
Annoyance is the most prevalent effect of aircraft noise. It
is important to note that while the overall, or average, community attitude
about a noise level is usually what is reported, some individuals will be much
more and others much less upset or annoyed with the sound in question. Figure 1.1 shows
this typical response pattern. This variation in response is what makes the
science of measuring "community response" a rather complicated
matter.
What are Other Principal Effects of Aircraft
Noise?
1. speech interference
2. sleep interference
3.
hearing damage risk
_ Ref 1
What are Some Less Frequently Identified Effects of Noise on
Humans?
1. physiological (cardiovascular and circulatory)
problems
2. psychological problems (stemming from intense
annoyance)
3. social behavioral problems
At the present time there
is no conclusive evidence to link these effects with aircraft noise. As
discussed in the text, these topical areas are often rife with conflicting
research results and are very controversial. The summary of the non-auditory
effects section (Section 8.0)
provides current guidance for interpreting these reported
effects.
What Other Areas May be Affected by Aircraft
Noise?
1. real estate values
2. land use
3.
wildlife
4. farm animals
While the reactions of animals to
noise have been studied, it is another research area plagued with widely varying
results. In all but extreme cases (such as in pristine wilderness or in the case
of excessive noise levels) wildlife and domesticated animals rarely display any
reactions to aviation noise.
How Do You Measure Aircraft
Noise?
sound is often measured using a sound level meter with a
filter which simulates the human hearing response. This filter and the human ear
give greater emphasis to sounds in the speech-important frequency bands and less
emphasis to the lower and higher frequencies. This differential response in the
human ear may have developed over the course of human evolution as a way to
filter the sounds of wind and water which might interfere with survival-related
communications such as "Here comes a Tyrannosaurus Rex--run for it!" In any
event, this filter is called the A-weighting filter, and the sound measured with
this filter is called the A-level (AL).
Now I Know What AL is, but I
Am Confused About "Energy Dose." What Exactly is the Sound Exposure Level
(SEL)?
When our sound level meter is measuring the AL, think of the
sound falling on the microphone like rain or snow. The maximum rate of rainfall
is the maximum AL. Now consider the sound level meter as a bucket or pail. After
the "noise event" has passed (aircraft flyover or truck passby) the rain or snow
collected in the bucket (having passed through the microphone) is the noise dose
or Sound Exposure Level (SEL). Essentially, loud noise events create a large
bucket (dose) of sound energy, while quieter events create smaller
buckets.
Now What Do I Do With "Buckets" of Noise (the Leq and
DNL)?
The buckets are typically collected over a 24-hour time period
and are poured into a large container. The total volume collected during the
24-hour time period is averaged to formulate a value called the "Equivalent
sound Level", or Leq. When the buckets collected during the nighttime hours are
multiplied by 10 (because of greater potential for disturbing people) and then
the volume averaged, we formulate a value called the "Average Day Night sound
Level" or DNL. The Leq and DNL are values one often encounters in looking at the
overall noise exposure from an airport operation.
-New Way of Rating Airport Noise. Sound and Vibration,
V.7,
No, 12, December 1973.
Section 2.0 NOISE METRICS
This section describes the noise metrics utilized
in conducting analyses of aircraft noise. While dozens of additional metrics
exist, this section focuses on the officially designated family of indices. A
working knowledge of these measures is extremely valuable in understanding the
remainder of this report.
AVIATION APPLICATIONS/ISSUES
1.
Correlation between human response and various measures of sound.
2.
Selection of the best metrics for specific applications.
3. Selection of
weighting factors for sound occurring at various times of day.
4.
Selection of metrics which are accurate, relatively easy to measure, compute and
understand.
GUIDANCE/POLICY/EXPERIENCE
1. The fundamental
sound level metric designated as the A-Weighted Sound Level, or AL. This metric
has often appeared in the literature as dBA. It is designated for measuring
noise at an airport and surrounding areas by Part 150.
2. Single event
dose or energy metric designated as the Sound Exposure Level or SEL.
3.
Airport yearly average noise exposure measure designated as the Yearly Average
Day Night Level or DNL. The DNL has often appeared in the literature as Ldn..
Required by Part 150 to measure the exposure of individuals to noise resulting
from the operation of an airport.
4. Effective Perceived Noise Level or
EPNL designated as the certification metric for large transport turbojet
aircraft and helicopters.
5. Time functions of ALm (such as Time Above,
TA and L-Values, L-10) identified as supplementary metrics for use in
environmental impact analyses.
6. Octave and one-third octave spectra
identified as important in specific applications such as sound proofing and
speech interference studies.
2.1 INTRODUCTION
The topic of noise
metrics has traditionally involved a rather confusing proliferation of units and
indices. In response to the requirements of the Aviation Safety and Noise
Abatement Act of 1979 (P.L 96-193), the FAA established a single system of
metrics for measuring and evaluating noise for land use planning and
environmental impact assessment. The FAA also has another system of metrics
which it employs for certification of commercial aircraft. This section
describes both systems of metrics. It also identifies other noise metrics
frequently and necessarily employed in noise certification and provides detailed
analysis of noise effects such as speech interference, hearing impact and sleep
disturbance.
Sound measures, or more academically, acoustical metrics,
all consist of three basic building blocks: 1) sound pressure level, expressed
in decibels, 2) frequency or pitch of the sound, and 3) time. The sound pressure
levels at various frequencies (points 1 and 2 above), for a given point in time,
are usually combined into a frequency spectrum (see Figure 2.1),
which is somewhat analogous to the fingerprint of the sound. This spectrum,
which varies with time, represents the real starting point for the metric
story (see Figure
2.2). From this point of origin, the following classes of metrics have
evolved:
(1) Single Event Maximum Sound Levels
The paragraphs below describe and
differentiate these four generic classes of acoustical metrics. An understanding
of these four classes essential for an individual undertaking a comprehensive
assessment of noise effects. (For mathematical formulations of each of the noise
metrics, the reader is referred to The Handbook of Noise Ratings (Ref. 1).
2.2 SINGLE EVENT MAXIMUM SOUND LEVEL METRICS
The
following noise metrics are generally related, each representing a maximum sound
level. The applications of these metrics are diagrammed in Figure 2.2.
2.2.1 A-Weighted Sound Level: ALm (Historically dBA),
Expressed in dB. The A-weighted Sound Level is the single event maximum
sound level metric. A-weighted sound pressure level is sound pressure level
which has been filtered or weighted to reduce the influence of the low and high
frequency extremes. Because unweighted sound pressure level does not correlate
well with human assessment of the loudness of sounds, various weighting networks
are added to sound level meters to attenuate low and high frequency noise in
accordance with accepted equal loudness contours. One of these weighting
networks is designated "A" (shown in Figure
2.3).

2.2.2
D-Weighted Sound Level: DLm (Historicall dB(D)), Expressed in dB.
D-weighted sound pressure level or D-level is sound pressure level which has
been frequency-filtered to reduce the effect of the low frequency noise and to
recognize the annoyance at higher frequencies. D-level is measured in decibels
with a standard sound level meter with contains a "D" weighting network with the
response curve shown in Figure 2.3. D-level
was developed as a simple approximation of perceived noise level (PNL) for use
in assess aircraft noise. PNL, addressed in the next paragraph, can be estimated
from the D-level by this equation: PNL = dB(D) + 7.
2.2.3 Perceived Noise Level (PNL), Expressed in dB.
Perceived Noise Level (PNL) is a rating of the noisiness that has been used
almost exclusively in aircraft noise assessment. PNL is computed from sound
pressure levels measured in octave or one-third octave frequency bands. This
rating is most accurate in estimating the perceived noisiness of broadband
sounds of similar time duration which do not contain strong discrete frequency
components. Currently it is used by the FAA and foreign governmental agencies in
the noise certification process for all turbojet -- powered aircraft and large
propeller-driven transports. The perceived noise level is expressed in decibels.
These units translate the subjective linearly additive noisiness scale to a
logarithmic dB-type
scale, where an increase of 10 dB in PNL is equivalent to a doubling of its
perceived noisiness.
2.2.4 Tone Corrected
Perceived Noise Level (PNLT), PNdB. Tone Corrected Perceived Noise Level is
basically the Perceived Noise Level adjusted to account for the presence of
discrete frequency components. PNLT was developed to aid in prediction of
perceived noisiness for aircraft flyovers and vehicle noise which contain pure
tones, or have pronounced irregularities in their spectrum. The method for
calculating PNLT adopted by the FAA involves calculation of the PNL of a sound
and the addition of a tone correction based on the tonal frequency and the
amount that the tone exceeds the noise in the adjacent one-third octave
bands.
2.3 SINGLE EVENT ENERGY DOSE
METRICS
The following noise metrics are generically related, each
representing a noise energy dose. Each metric reflects both the maximum sound
level and the duration of the event. As shown in Figure 2.2, these
metrics are derived from single event sound level metrics.
2.3.1 Effective Perceived Noise Level (EPNL), Expressed in
dB or EPNdB. Effective Perceived Noise Level is a single number measure of
complex aircraft flyover noise which approximates human annoyance responses. It
is derived from PNL and PNLT and includes correction terms for the duration of
an aircraft flyover and the presence of audible pure tones or discrete
frequencies (such as the whine of a jet aircraft) in the noise signal. The EPNL
is used by the FAA as the noise certification metric for large transport and
turbojet aircraft and helicopters.
2.3.2 Sound
Exposure Level (SEL), Expressed in dB. SEL is a measure of the effect of
duration and magnitude for a single event measured in A-weighted sound level
above a specified threshold which is at least 10 dB below the maximum value. In
typical aircraft noise model calculations, SEL is used in computing aircraft
accoustical contribution to the Equivalent Sound Level (Leq) and the Day-Night
Sound Level (DNL).
2.4 CUMULATIVE ENERGY AVERAGE
METRICS
The cumulative energy average noise metrics are usually
derived from single event energy dose metrics. These metrics can also be
computed from continuous noise measurement data. Cumulative metrics correlate
well with aggregate community annoyance response. They were not designed as
single source measures, so they do not account adequately for tonal components.
Nor do they relate accurately to speech interference, sleep disturbance or other
phenomena requiring analysis using single event maximum and energy dose sound
level data. In practice, these measures are not used in determining source
standards or for certification of product noise.
2.4.1 Equivalent Sound Level (Leq), Expressed in dB.
Equivalent sound level, Leq, is the energy average noise level (usually
A-weighted) integrated over some specified time. Equivalent signifies
that the total
2.4.3
Community Noise Equivalent Level (CNEL), in dB. CNEL, like DNL,
incorporates the energy average A-weighted sound level integrated over a 24-hour
period Weightings are applied for the noise levels occurring during the evening
(7 p.m. - 10 p.m.) and nighttime (10 p.m. - 7 a.m.). CNEL differs from DNL in
the addition of the evening weighting step function of 3 dB which is intended to
account for activity interference and annoyance during that time period. It was
originally used by the state of California, but it is being phased
out.
2.4.4 Noise Exposure Forecast (NEF), in
dB. Noise Exposure Forecast performs the same role as DNL or CNEL but is
developed using EPNL as the intermediate single event dose metric. The NEF
metric incorporates a weighting factor which effectively imposes a 12.2 dB
penalty on sound occurring between 10 p.m. and 7 a.m. This corresponds to a
nighttime event multiplier of 16.7. NEF correlates extremely well with DNL and
the equivalency DNL = NEF + 35 is often used.
2.5
CUMULATIVE TIME METRICS
2.5.1 24-Hour
Time Above (TA), Expressed in Minutes. The 24-hour TA metric provides the
duration in minutes for which aircraft related noise exceeded specified
A-weighted sound levels. An example of a TA contour is shown in Figure 2.4. TA is
one of the criteria specified in HUD Circular 1390.2 for determining eligibility
for HUD construction funding (Ref. 3). TA'S
inverse, the L-value (e.g., L 10) is used (along with Leq) as the FHWA criteria
for planning and design of Federal-aid highways. Further, TA can be related
directly to some "threshold activated" physiological or annoyance effects.
2.5.2 Day, Evening, Night (TA), Expressed in
Minutes. The Day-TA metrics provide the duration in minutes for which
aircraft related noise exceeded specified A-weighted sound levels during the
period 7:00 a.m. to 7:00 p.m. The Evening TA metrics provide the duration in
minutes for which aircraft related noise exceeded A-weighted sound levels during
the period from 7:00 p.m. to 10:00 p.m. The Night TA metrics provide the
duration in minutes for which aircraft related noise exceeded A-weighted sound
levels during the period from 10:00 p.m. to 7:00 a.m.
2.6 DNL: THE STANDARD CUMULATIVE AVERAGE ENERGY
METRIC
The FAA selected DNL as the cumulative average energy metric
to be used in airport noise exposure studies. While a dialogue continues within
research circles concerning weighting functions, the DNL has emerged as a sound
and workable tool for use in land use planning and in relating aircraft noise to
community reaction. The substantiating basis for the DNL can perhaps best be
summarized as follows:
2) The nominal 10 dB decrease in ambient noise levels
in many residential areas at nighttime provides a sensible basis for the
weighting factor.
2.7 EVALUATION OF THE DNL METRIC
FOR HELIPORT/HELISTOP NOISE IMPACT ASSESSMENT
With the increase in
helicopter operations in and around urban areas, the FAA has sought to include
helicopters in the environmental planning process. In this context, the question
has arisen of whether or not the average cumulative energy metric DNL, which is
used in the analysis of noise from conventional aircraft, would also be
appropriate for analysis of helicopter noise. Most commercial airports have
hundreds of operations a day, while heliports generally handle fewer than
thirty. The metric used to analyze helicopter noise would have to be sensitive
enough to accurately reflect community response at comparatively low levels of
noise exposure (lower cumulative levels because of fewer flights).
In
order to investigate whether or not DNL would be appropriate, the FAA supported
a field test program to examine subjective response to helicopter operations.
The actual study was conducted by NASA Langley Research Center and is summarized
below (Ref. 4).
In the study, researchers examined the reaction of community residents to low
numbers of helicopter noise events. Residents of the selected community were
interviewed twenty-three times about their general noise annoyance on particular
days. Unknown to them, on those days helicopter flights had been controlled for
the test purpose; the number of flights per day varied from 0 to 32. The
exposure varied randomly through each of the
|
METRIC |
DESCRIPTION |
|
One-third Octave Sound Pressure Levels |
The one-third octave band sound pressure levels are the starting point for all other metrics; useful in implementation of soundproofing |
|
PNL |
Sound Level from which EPNL was developed |
|
PNLT |
Sound Level from which EPNL was developed |
|
EPNL |
A maximum sound level single event cumulative metric developed from the PNLT and PNL sound level. Used in FAR Part 36, Appendix C Certification, Advisory Circular 36-lB and Advisory Circular 36-2A. |
|
NEF |
An Airport cumulative metric no longer in use in the U.S. but often used in older studies; replaced by DNL (the FAA approved metric) |
|
Alm |
A sound level metric applied as follows:
1050.lC Analysis FAR Part 36 Appendix F Certification Specific eligibility for Soundproofing Implementation of Soundproofing Noise Monitoring Systems FAA Advisory Circular |
|
TA |
An airport cumulative metric derived from dB(A) and applied as follows:
l050.lD Analysis Noise Monitoring Systems |
|
Lx |
An airport Cumulative metric derived from dB(A) and applied as follows:
l050.lD Analysis Noise Monitoring Systems |
|
SEL |
A maximum sound level, single event cumulative metric derived from dB(A) and applied as follows:
Noise Monitoring Systems |
|
Leq |
An airport cumulative metric derived from SEL; no application in aviation |
|
DNL |
An airport cumulative metric derived from SEL with the following applications:
Airport Noise Analysis FAR l050.lD Analysis General Eligibility for Soundproofing Noise Monitoring Systems |
|
CNEL |
An airport cumulative metric derived from SEL used only by the state of California; CNEL will be phased out in the next few years. |
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twenty-three (non-consecutive) test days. It was found that the (1) maximum
noise level, (2) the number of noise events, and (3) the duration of the events
(reflected in cumulative energy noise indices) correlated well with community
annoyance response.
The results of this program provided strong evidence
that the same analytical tool, the DNL metric, employed at airports with large
numbers of operations can be used with confidence in assessing the environmental
impact (human response) of comparatively small numbers of helicopter
operations.
2.8 SUMMARY OF NOISE METRIC
POLICY
The FAA noise metric usage policy is presented in Figure 2.2. The
figure shows the genealogy of the various types of metrics starting from the
one-third octave sound pressure level data. The dBA, PNL and PNLT are identified
as pertinent sound levels. SEL and EPNL are identified as significant
single event cumulative energy (or dose) metrics while Leq, DNL, CNEL and
NEF are recognized as airport cumulative exposure metrics along with TA
and Lx. The policy outline reflects the stated position supporting ALm as the
single event maximum sound level metric, SEL as the single event dose metric,
and DNL as the airport cumulative noise metric. EPNL is retained as a
certification noise metric. The SEL, TA and Lx metrics are all descendants of
the A-weighted sound level and their use is consistent with stated
policy.
2.9 NOISE METRICS
APPLICATIONS
Each of the noise metrics discussed above has a specific
set of applications for which it is most appropriate, as detailed in Table 2.1.
Top
2.
Hassall, J.R. and K. Zaveri. Acoustic Noise Measurements. Bruel &
Kjaer, January 1979.
3. Housing and Urban Development
Circular 1390.2.
4. Fields, James M. and Clemans A.
Powell. Community Survey of Helicopter Noise Annoyance Conducted Under
Controlled Noise Exposure Conditions. Unpublished Report, December 1984.
Top
Section 3.0 ANNOYANCE AND AIRCRAFT NOISE
INTRODUCTION
The typical response of humans to aircraft noise
is annoyance. Annoyance response is remarkably complex and, considered on an
individual basis, displays wide variability for any given noise level.
Fortunately, when one considers average annoyance reactions within a community,
one can develop aggregate annoyance response/noise level relationships. This
section introduces the reader to the factors which influence individual
annoyance response. Also included are examples of research findings which
display aggregate community annoyance responses.
AVIATION
APPLICATION/ISSUES
Annoyance is the number one consequence of
excessive aircraft noise. The continued growth of the aviation industry and
expansion of airport capacity is in part dependent on how well noise
compatibility planning is
handled.
GUIDANCE/POLICY/EXPERIENCE
It is the charter of
the FAA to assure safety and promote civil aviation. Promoting civil aviation
means, among other things, addressing the problems of aircraft noise annoyance.
The FAA, working with other members of the community, has taken a series of
steps designed to bring about greater compatibility between aircraft noise
levels and affected individuals. Actions include:
1. Source noise
certification regulations
2. FAR Part 150 Airport Noise Exposure / Land Use
Compatibility Planning Process
3. Research into the mechanism of annoyance to
aircraft noise
4. Advisory publications designed to mitigate aircraft noise
impact on noise sensitive areas.
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3.1 INTRODUCTION
Responses of annoyance
are the most common reaction to aircraft noise. This section discusses, first,
how people perceive noisiness, and second, some of the emotional and physical
variables which may influence an individual's response to a sound. A review of
pertinent research concludes this section.
3.2
PERCEPTION OF NOISE
How people perceive loudness or noisiness of
any given sound depends on several measurable physical characteristics of the
sound. These factors are:
A. Intensity. In general, a ten decibel
increase in intensity may be considered a doubling of the perceived loudness or
noisiness of a sound; however, other psychoacoustic evidence suggests that a
somewhat greater than IO decibel increase in peak level of airplane flyover
noise is required to produce a perceived doubling of loudness.
B.
Frequency Content. Sounds with concentration of energy between 2,000 Hz
and 8,000 Hz are perceived to be more noisy than sounds of equal sound pressure
level outside this range.
C. Changes in Sound Pressure Level.
Sounds that are increasing in level are judged to be somewhat louder than those
decreasing in level (consider police and emergency vehicle sirens).
D.
Rate of Increase of Sound Pressure Level. Impulsive sound (ones reaching
a high peak very abruptly, such as pile drivers or jack hammers) are usually
perceived to be very noisy.
3.3 VARIABLES
AFFECTING RESPONSE
Individual human response to noise is subject to
considerable natural variability, over the past 35 years, researchers have
identified many of the factors which contribute to the variation in human
reaction to noise.
3.3.1 Emotional
Variables. Knowledge of the existence of these individual variables helps to
understand why it is not possible to state simply that a given noise level from
a given noise source will elicit a particular community reaction or have a
certain environmental impact. In order to do that, it would be necessary to know
how much each variable contributes to human reaction to noise. Research in
psychoacoustics has revealed that an individual's attitudes, beliefs and values
may greatly influence the degree to which a person considers a given sound
annoying. The aggregate emotional response of an individual to noise has been
found to depend on:
A. Feelings about the Necessity or Preventability
of the Noise. If people feel that their needs and concerns are being
ignored, they are more likely to feel hostile towards the noise. This feeling of
being
Top alienated or of being ignored and abused is the root of many human annoyance
reactions. If people feel that those creating the noise care about their welfare
and are doing what they can to mitigate the noise, they are usually more
tolerant of the noise and are willing and able to accommodate higher noise
levels.
B. Judgment of the Importance and Value of the Activity which
is Producing the Noise. If the noise is produced by an activity which people
feel is vital, they are not as bothered by it as they would be if the
noise-producing activity was considered superfluous.
C. Activity at
the Time an Individual Hears a Noise. An individual's sleep,, rest and
relaxation have been found to be more easily disrupted by noise than his
communication and entertainment activities.
D. Attitudes about
Environment. The existence of undesirable features in a person's residential
environment will influence the way in which he reacts to a particular
intrusion.
E. General Sensitivity to Noise. People vary in their
ability to hear sound, their physiological predisposition to noise and their
emotional experience of annoyance to a given noise.
F. Belief about
the Effect of Noise on Health. The extent to which people believe that
exposure to aircraft noise will damage their health affects their response to
aviation noise.
G. Feeling of Fear Associated with the Noise. For
instance, the extent to which an individual fears physical harm from the source
of the noise will affect his attitude toward the noise.
A. Type of
Neighborhood. Instances of annoyance, disturbance and complaint associated
with a particular noise exposure will be greatest in rural areas, followed by
suburban and urban residential areas, and then commercial and industrial areas
in decreasing order. The type of neighborhood may actually be associated with
one's expectations regarding noise there. People expect rural neighborhoods to
be quieter than cities. Consequently, a given noise exposure may produce greater
negative reaction in a rural area.
B. Time of Day. A number of
studies has suggested that noise intrusions are considered more annoying in the
early evening and at night than during the day.
C. Season. Noise
is considered more disturbing in the summer than in the winter. This is
understandable since, during the summer, windows are likely to be open and
recreational activities take place out of doors.

Top D. Predictability of the Noise. Research has revealed that individuals
exposed to unpredictable noise have a lower noise tolerance than those exposed
to predictable noise.
E. Control over the Noise Source. A person
who has no control over the noise source will be more annoyed than one who is
able to exercise some control.
F. Length of Time an Individual Is
Exposed to a Noise. There is little evidence supporting the argument that
annoyance resulting from noise will decrease with continued exposure; rather,
under some circumstances, annoyance may increase the longer one is
exposed.
The inherent variability in the way individuals react to
noise makes it impossible to predict accurately how any one individual will
respond to a given noise. However, when one considers the community as a whole,
trends emerge which relate noise to annoyance. In this way it is possible to
correlate DNL with community annoyance. This measure will represent the average
annoyance response for the community.
In any community there will be a
given percentage of the population highly annoyed, a given percentage mildly
annoyed and others who will not be annoyed at all. The changing percentage of
population within a given response category is the best indicator of noise
annoyance impact.
Various studies have focused on the relationship
between annoyance and noise exposure, one researcher, in analyzing the results
of numerous social surveys conducted at major airports in several countries,
derived the curves shown in Figure 3.1 relating
degree of annoyance and percent of population affected with noise exposure
expressed in DNL (Ref. 1). A survey
conducted in the Netherlands investigated the relationship between the DNL and
the percentage of those questioned who suffered feelings of fear, disruption of
conversation, sleep or work activities (Ref. 2). Figure 3.2 reflects
these findings.
In 1960 the "Wilson Committee" was appointed by the
British Government to investigate the nature, sources and effects of the problem
of noise (Ref.
3). The final report, published in 1963, included results of extensive
examination of community response to aircraft operations at London Heathrow
Airport. Figure
3.3, adapted from that report, shows the relationship between DNL and the
percent of the population disturbed in various activities including sleep,
relaxation, conversation and television viewing. Disturbance response categories
for startle and house vibration are also included.
The EPA publication
"Information on Levels of Environmental Noise Requisite to Protect Health and
Welfare with an Adequate Margin of Safety" provides a relationship between the
percent of population highly annoyed and the Day-Night Sound Level (DNL) (Ref. 4). These data
are shown in Figure
3.4, along with the relationship between annoyance, complaints and community
reaction.


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3.5 CONCLUSION
This section has presented a
series of relationships useful in interpreting average community response to
aircraft noise. These data should provide the reader with the necessary
perspective to begin understanding the human reactions to various levels of
cumulative noise exposure (DNL).
1. Richards, E. J, and J. B. 0llerhead. Noise Burden
Factor - New Way of Rating Airport Noise. Sound and Vibration, V. 7,
No, 12, December 1973.
2. Kryter, Karl D. The
Effects of Noise on Man. New York, Academic Press, 1970.
3. Great Britain Committee on the Problem of Noise. Noise, Final
Report. Presented to Parliament by the Lord Minister for Science by Command of
Her Majesty. London, H. M. Stationery Office, July 1963.
4. U.S. Environmental Protection Agency, Office of Noise
Abatement and Control, Washington, D.C. Information on Levels of Environmental
Noise Requisite to Protect Public Health and Welfare with an Adequate Margin of
Safety. March 1974.
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Section 4.0 DIFFERENT SOURCES/DIFFERENT HUMAN
RESPONSE?
INTRODUCTION
This section addresses a fundamental question
raised from time to time in connection with aviation noise related law suits,
environmental impact assessments, and research studies. It has been suggested
that aircraft noise levels should be treated as more annoying to people than the
same sound levels generated by other sources. A review of the research shows
that very strong positions have been taken both supporting and opposing the
theory. The most recent papers appearing in the scientific journals concede that
a differential in response may exist but it can not be shown to be statistically
significant.
AVIATION APPLICATIONS/ISSUES
Should aircraft
noise be considered as comparable to noise from other sources in the land use
planning and environmental assessment
process?
GUIDANCE/POLICY/EXPERIENCE
In the general
application of noise exposure/land use criteria, aircraft noise should be
considered in the same manner as noise from other sources.


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4.1 INTRODUCTION
In assessing comparative
contributions to the overall annoyance with noise experienced by an individual,
the issue of whether or not aircraft noise should be compared with other ambient
sources continues to arise. The issue is an important one in terms of
establishing acceptable cumulative noise exposure levels for various land use
categories. This section reviews current literature on this controversial
topic.
4.2 SCHULTZ - KRYTER DEBATE
In
1978, Theodore Schultz published an article synthesizing results from many
social surveys on noise annoyance. In this article he stated that it is possible
to compare aircraft and other transportation noise equally, and to find and use
a median annoyance response curve for them (Ref. 1). In order
to compare these various results, Schultz developed some theories and formulas
with which he determined which parts of each survey would fall into the "highly
annoyed" category. He also figured the DNL indices for these surveys and plotted
them (see Figure
4.1). Figure
4.2 reproduces Schultz's "synthesis curve", the median of all the noise
surveys.
Karl Kryter, responding in 1982 to Schultz's article, proposed a
different relationship (Ref. 2).. While
Schultz only considered people who were highly annoyed, Kryter stated that all
individuals annoyed should be considered in these comparisons. He also developed
the DNL values for each study differently, so his values varied significantly
from those of Schultz. Kryter also attempted to explain the poor correlation
between noise exposure and annoyance in individuals by explaining that, while it
is assumed that noise exposure is homogeneous over a given neighborhood, an
individual's particular dose of noise may vary quite a bit.
Kryter cited
Grandjean (Ref.
3), another researcher who found that aircraft noise is significantly more
disturbing than other noise. This Swiss study stated that it took a DNL of 10 to
15 dB higher for road traffic noise to cause equal disturbance as aircraft.
Kryter then explained his concept of the "effective exposure" of noise, rather
than the exposure that may actually be measured or reported. Kryter suggests
that because aircraft noise falls over a structure, like a house, equally, as
opposed to passing through interfering structures as traffic noise would do (as
in moving from the front to the back of a house), the "effective noise exposure"
would be greater than that of traffic noise. Kryter further submits that, for a
house facing the road, residents in the back yard would experience diminished
noise from those in the front yard; however, they would all experience equal
aircraft noise. Likewise, each room in the house would experience nearly
identical exposure to aircraft noise (Kryter evidently only considered single -
level homes). Kryter found a front to back of house difference of 17 - 21 dB for
road traffic and only 0.3 dB for aircraft noise. Thus, Kryter suggests that
aircraft noise must be considered separately from other transportation
noise.

Top
Fortunately, other researchers have examined this topic; their views aid in
going past the Schultz - Kryter stalemate.
4.3
HALL'S RESEARCH AND ANALYSIS
In 1981, Fred Hall reported on data
which had been collected around the Toronto International Airport (Ref. 4). For the
first time, data had been collected on both aircraft and ground traffic noise
using comparable questions and measured in DNL, thus alleviating the need for
juggling survey results to fit DNL, as Kryter and Schultz had to do. His
conclusion was that there is indeed a difference between community responses to
aircraft noise and to road traffic noise when each is measured by DNL. Figure 4.3 relates
his findings in relation to Schultz's synthesis curve; Hall notes that the
aircraft noise curve falls out of proportion with the others.
For the same noise level, a greater percentage of
people are highly annoyed by aircraft noise. The
difference in annoyance at the two sources is not
constant but instead increases as Ldn increases. The
difference in annoyance is equivalent to about 8 dB at
Ldn of 55 dB increasing to about 15 dB at Ldn of 65 dB.
Hall puts forth some possible explanations of these variations. For example,
the sporadic time pattern of aircraft noise differs from the relatively steady
noise of road traffic. Thus, maximum levels for aircraft noise will be higher.
Hall suggests that until further work can be done, "Ldn is a reasonable
predictor of response to any particular source, but there are differences in
response to different sources at the same Ldn value." Hall concluded that the
best thing to do, then, would be to use separate functions to estimate community
response to different types of noise.
In a later article (published in
December 1984), Hall further addressed this complex issue, substantially
altering his previous conclusions (Ref. 5). He
references about a dozen papers published on this subject over the last five
years. Hall suggests that intrinsic differences may exist but can not be
substantiated as statistically significant. His summary statements are excerpted
below:
The overwhelming conclusion from the recent literature is that different studies have led to different dose-response functions. This has happened for different sources, for different types of one source, and even for different studies at the same location (e.g., Heathrow). There is some consistency of evidence that the annoyance response function for rail noise is lower than for road or aircraft noise. (Rohrmann reaches the same conclusion in his review of relevant literature.) There is also some indication, but with fewer studies pertaining to it, that the aircraft annoyance function is higher than that for road traffic. However, the evidence is not strong enough to totally reject the hypothesis that all of this is just random variation about the "average" response.
Top Lastly, an "average" dose-response function appears to be useful in two
contexts, both defined by limited information. The first is the general
situation we are now in, in which it appears that different dose-response
functions are warranted, but we cannot specify precisely the conditions calling
for each. Although we suspect the variance in results is not simply random, it
almost behaves as if it were, in which case the "average" function represents
our best current estimate. The second situation will arise in the future, when
we may be able to specify clearly the conditions calling for separate
dose-response functions. Even then, there will undoubtedly be conditions which
we cannot categorize, in which case again the "average" response function would
be. the best one to use.
For matters of policy, there does not exist at this
time enough evidence to support the requirement of a differential for comparing
aircraft noise with noise from other sources. All transportation and other
ambient noise sources therefore can be treated as comparable when considering
aviation noise impact.
1. Schultz, Theodore. Synthesis of Social Surveys on Noise
Annoyance. J. Acoust. Soc. Am. 64, 1978.
2.
Kryter, Karl D. Community Annoyance from Aircraft and Ground Vehicle Noise.
J. Acoust. Soc. Am. 72 (4), October 1982.
3.
Grandjean, P. Graf, A. Lauber, H.P. Meier, and R. Huller. Survey on the Effects
of Aircraft Noise in Switzerland. Inter-Noise 76, Washington, D.C., April
1976.
4. Hall, Fred L., Susan E. Bernie, Martin
Taylor, and John E. Palmer. Direct Comparison of Community Response to Road
Traffic Noise and to Aircraft Noise. J. Acoust, Soc. Am. 70 (6), December
1981.
5. Hall, Fred L. Community Response to Noise: Is
All Noise the Same? J. Acoust. Soc. Am. 76 (4), October 1984.
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Section 5.0 HEARING and HEARING LOSS
INTRODUCTION
This section describes the human hearing mechanism
and the processes of temporary and permanent hearing loss. The results of
research are presented and the potential for hearing loss in aviation noise
environments evaluated. OSHA hearing protection criteria are also
addressed.
AVIATION APPLICATIONS/ISSUES
1. Permanent or
temporary hearing loss.
a. cockpit crew
b. flight attendants
c.
passengers
d. persons in communities exposed to
aircraft
overflight
2. Temporary hearing loss for the same categories
of individuals listed above.
GUIDANCE/POLICY/EXPERIENCE
1.
FAA-sponsored research results show that permanent hearing loss is not a
likelihood for a) cockpit crew, b) flight attendants, c) passengers, d) people
exposed to overflights.
2. Temporary hearing loss (up to several hours
recovery time) may occur in commercial aviation noise environments. These
temporary sensitivity shifts are not unusual in the industrial setting and do
not exceed OSHA criteria.
3. Persons on the ground exposed to aircraft
overflights would typically not experience any temporary hearing loss due to the
relatively short duration of the noise exposure.
4. A greater degree of
temporary and possible permanent hearing loss can result in the case of long
exposure times in certain small propeller driven aircraft.

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5.1 INTRODUCTION
It is well established
that continuous exposure to high levels of noise will damage human hearing. This
section begins with a description of the hearing mechanism, followed by
discussion of the effects of noise on hearing, along with criteria for hearing
protection established by the military, the FAA and OSHA. Finally, methods for
protection of hearing are discussed.
5.2 THE
HEARING MECHANISM
The ear is an external sense organ designed to
receive and respond to air-borne acoustic vibratory energy. Figure 5.1 provides
a schematic cross section showing the outer, middle and inner ears. The external
ear, made up of the auricle (the outer portion of the ear) and the ear canal,
transmits sounds to the eardrum. The eardrum, which is a very thin membrane that
moves very slightly in response to sound pressure levels, separates the ear
canal from the middle ear.
The middle ear is an air-filled cavity that
lies between the outer and the inner ear (see Figure 5.2). It
acts as a mechanical amplifier of the air pressure vibrations from the eardrum
and through a series of bones called the ossicles. Air pressure vibrations
displace the eardrum, which then displaces the ossicles, a link of three small
bones which reach across the middle ear cavity to the delicate, fluid-filled
membranes of the inner ear. The ossicles, made up of the malleus, the incus and
the stapes, rest against the opening to the inner ear, the oval window; when the
ossicles are displaced, the stapes pushes through the oval window, displacing
the fluid in the inner ear.
The middle ear allows pressure variations in
air to be transmitted into pressure variations in fluid with very little loss of
energy. This is due in part to the relative size difference between the eardrum
and the oval window (the eardrum has an area 20 times that of the oval window).
Thus, the force exerted on the inner ear fluid by the stapes is about the same
as the force exerted on the eardrum by the sound wave in the air, but the
resulting pressure is much greater -- as much as a ratio of 22 to 1.
The
inner ear contains the final section of the organ of hearing, the cochlea, which
rests, coiled like a snail, against the oval window. As the stapes forces the
oval window in and out, the fluid of the cochlea is also moved. About thirty
thousand hair cells (called cilia) located in the cochlea react to the fluid
motions, translating them to nerve impulses (and converting them from mechanical
to electrical energy), then transmitting the impulses to the brain for
interpretation.
Acoustical energy may also be conducted to the inner ear
through vibration of bone. An example is the sound of one's own voice.
Bone-conducted vibrations set up similar patterns of vibration of the cochlear
partition as does air-conducted sound.
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5.3 AUDITORY RANGE
The ear is capable of
hearing a frequency range of about nine octaves and a dynamic range of more
than120 dB. The least pressure needed to make a tone audible (the "threshold
pressure") depends on the frequency of the tone. The lower frequency limit of
hearing is a vague boundary because hearing merges into the sensation of
vibration; the upper intensity limit of hearing is sometimes taken as the
threshold of discomfort, which is a sound pressure level of about 120 dB
(independent of frequency). At 120 dB, there may be a sensation of tickling in
the middle ear. However, the threshold of pain appears to be 140 dB, with sound
continuing to sound louder, with increasing pressure, until auditory fatigue or
acoustical injury is reached.
5.4 EFFECTS OF NOISE
ON HEARING
The sensitivity of the ear is not constant with frequency.
Both the threshold at which a tone can be heard and how loud it sounds may vary
considerably as a result of previous exposure to sounds of the same or of
different frequencies. Even sounds below 90 - 100 dB may bring about short-term
changes in hearing; these changes, however, are simply adjustments of the
balance within the ear, much like the process of light or dark adaptation in the
eye.
Other sounds may produce longer-lasting changes in the threshold of
hearing; the chances of these changes occurring increase with continuing
exposure to loud noise. The three principle effects are:
1. temporary
reduction in hearing acuity, which is referred to as temporary threshold shift
(TTS)
2.
permanent hearing loss referred to as a "Noise Induced Permanent Threshold
Shift" or NIPTS
3.
ringing in the ears, or tinnitus
5.4.1 TTS.
A temporary threshold shift is a common effect of noise on hearing in noisy
industrial and entertainment situations. When an individual is tested for
hearing acuity, an audiometer is used to establish the lowest levels of sound
that person can perceive at different frequency bands. After exposure to high
noise levels for a short time, or moderate noise levels over a long time, the
minimum level that the person can perceive may shift to a higher level.
Temporary shifts of 20 to 30 dB are usual in healthy ears in noisy situations
with a typical eight-hour exposure. This shift is only temporary, however; a
100% recovery of the pre-noise exposure hearing acuity usually occurs within
several hours. TTS is also known as "auditory fatigue."
5.4.2 NIPTS. NIPTS, or noise induced permanent
threshold shift, is just that -- the minimum level at which a person can
perceive sound permanently shifts to a higher level. In layman's terms, a person