Пресс-релиз популярных книг
.
Авторы: 111 А Б В Г Д Е Ж З И Й К Л М Н О П Р С Т У Ф Х Ц Ч Ш Щ Э Ю Я
Книги: 164 А Б В Г Д Е Ж З И Й К Л М Н О П Р С Т У Ф Х Ц Ч Ш Щ Э Ю Я
На сайте 111 авторов, 92 книг, 72 статей, 5913 глав.
6.9 AIRCRAFT NOISE CRITERIA
The noise of automobile and truck traffic along a freeway is relatively uniform,
with a few highs and lows in the noise level. On the other hand, the
noise due to the fly-over of aircraft from an airport is neither constant nor
uniform, even near the airport. Some large airports have takeoffs and landings
as frequently as one every minute or two, whereas smaller airports may
have only one or two takeoffs and/or landings each hour. The intrusive
noise of the aircraft may be as much as 30–40 dBA higher than the ambient
noise, in contrast to ground traffic noise. The intrusive noise for aircraft is
often more annoying than the more steady ground traffic noise, so different
methods have been examined to determine the effect of aircraft noise.
Acoustic Criteria 255
Copyright © 2003 Marcel Dekker, Inc.
6.9.1 Perceived Noise Level
The perceived noise level, LPN, was developed as a single-number rating of
annoyance to noise, or aircraft noise, in particular (Kryter, 1959). The
perceived noise level is developed from contours of equal perceived ‘‘noisiness’’
(Kryter and Pearsons, 1963). The units for the equal ‘‘noisiness’’
contours is called noys, in analogy with an older procedure of determining
contours for equal ‘‘loudness’’ in sones (Fletcher and Munson, 1933;
Stevens, 1972). The numerical values of the noys are selected such that a
noise of 4 noys is perceived as four times as ‘‘noisy’’ as a noise of 1 noy. The
conversion data needed for converting from octave band sound pressure
level measurements to an effective noy value are given in Table 6-20
(Pinto, 1962).
The procedure to obtain an effective perceived noise level, LEPN,
dB(PN), from experimental octave band sound pressure level data is as
follows. First, the octave band data is converted to noys using Table 6-20.
Next, the effective noy value Ne is calculated from the following expression:
Ne ј 0:3_Nj ю 0:7Nmax (6-13)
256 Chapter 6
TABLE 6-20 Contours of Equal Noisiness N, in noys
N, noys
Octave band center frequency, Hz
63 125 250 500 1,000 2,000 4,000 8,000
1 60 51 44 40 40 32 29 37
2 67 59 53 50 50 42 39 44
3 72 64 59 56 56 50 44 49
5 77 71 66 63 63 55 52 57
10 85 79 75 73 73 65 62 67
15 90 85 81 79 79 71 68 73
20 94 89 85 83 83 75 72 77
30 100 95 91 89 89 81 78 83
40 104 99 95 93 93 87 82 87
50 108 103 99 96 96 89 86 91
60 110 105 101 99 99 91 88 93
80 114 109 105 103 103 96 93 98
100 117.5 112.5 108.5 106.5 106.5 99 96 101
150 123 118 114 112 112 105 102 107
200 127.4 122.4 119.4 116.4 116.4 109 106 111
300 133.3 128.3 124.3 122.3 122.3 115 112 117
Source: Pinto (1962).
Copyright © 2003 Marcel Dekker, Inc.
The first term is the sum of the noy values for the octave bands, and Nmax
is the largest noy value in all of the octave bands. Finally, the effective
perceived noise level, LEPN, is determined from the following relationship:
LEPN ј 40 ю
10log10 Ne
log10р2Ю
(6-14)
It is noted that an increase of 10 dB(PN) is equivalent to a doubling of the
noisiness in noys.
Example 6-9. The sound level spectrum for a single fly-over at a particular
location around an airport is given in Table 6-21. Determine the effective
perceived noise level for the noise.
The noisiness values corresponding to each octave band sound pressure
level are determined from Table 6-20 and listed in Table 6-21. The
largest noy value or Nmax value is 74 noy; this occurs in the 250 Hz octave
band.
The effective noisiness is calculated from Eq. (6-13):
Ne ј р0:3Юр24 ю 47 ю 74 ю 56ю_ _ _Ююр0:7Юр74Ю ј р0:3Юр327Ю ю 51:8
Ne ј 149:9 noy
The effective perceived noise level is found from Eq. (6-14):
LEPN ј 40 ю
10 log10р149:9Ю
log10р2Ю ј 40 ю 72:2 ј 112:2dBрPNЮ
6.9.2 Noise Exposure Forecast
The noise exposure forecast (NEF) was developed to determine the land-use
compatibility around a commercial (not military) airport with the noise
generated by the aircraft using the airport (Galloway and Bishop, 1970).
The aircraft noise is usually much more significant than any other noise
source for those people living in the vicinity of the airport.
Acoustic Criteria 257
TABLE 6-21 Data for Example 6-9
Octave band center frequency, Hz
63 125 250 500 1,000 2,000 4,000 8,000
Lp(OB), dB 97 102 104 98 90 85 80 76
Nj , noy 24 47 74a 56 32 40 35 19
aNmax value.
Copyright © 2003 Marcel Dekker, Inc.
For a specific class of aircraft (i) on one of the flight paths р jЮ of the
airport, the noise exposure forecast, NEFрi; jЮ, is related to the effective
perceived noise level, LEPNрi; jЮ, and the number of daytime and nighttime
flights, ND and NN. A landing is considered as one ‘‘flight,’’ and a takeoff is
considered as another ‘‘flight’’ in determining the NEF:
NEFрi; jЮ ј LEPNрi; jЮю10 log10ЅNDрi; jЮю16:67NNрi; jЮ__88 (6-15)
The value of NDрi; jЮ is the number of flights between 7:00 a.m. and 10:00
p.m. (daytime), and NNрi; jЮ is the number of flights between 10:00 p.m. and
7:00 a.m. (nighttime), for a particular class of aircraft (i) and a specific flight
path ( j). The factor 16.67 arises fromthe fact that the ratio of daytime hours
to nighttime hours is р15=9Ю ј 1:667, and the noise during the nighttime
hours is weighted as 10 times as important as the daytime noise. The constant
88 is arbitrary; however, it was introduced to avoid confusion between
the NEF and the composite noise rating, used previously for rating aircraft
noise effects.
Values for the effective perceived noise level for various types of aircraft
and the detailed method for calculation of this parameter from measurements
are outlined in the literature (Pearsons and Bennett, 1974).
The NEF value at a specific location adjacent to the airport is found
by adding (energywise) the NEFрi; jЮ for each class of aircraft along each
flight path:
NEF ј 10log10
X
i
X
j
10NEFрi;jЮ=10
" #
(6-16)
For a rough approximation (within 3 dBA), the NEF can be calculated
from measured values of the day–night level (EPA, 1974):
NEF _ LDN _35 (6-17)
Noise exposure forecast contours have been used by HUD in evaluating
prospective land use around airports. The report on the determination of
the NEF contours is usually included in environmental impact studies dealing
with the noise from the aircraft operations around an airport area.
Representative land-use compatibility recommendations are given in
Table 6-22. The criteria of the U.S. Department of Housing and Urban
Development (HUD) are shown in Table 6-23 (HUD, 1971).
The detailed construction of the NEF contours for a specific airport is
a time-consuming process. An approximate procedure has been developed
to estimate the location of the NEF-30 and NEF-40 contours, based on the
flight schedules for the airport (HUD, 1971). The dimensions of the approximate
NEF-30 and NEF-40 contours are illustrated in Fig. 6-4. The numer-
258 Chapter 6
Copyright © 2003 Marcel Dekker, Inc.
Acoustic Criteria 259
TABLE 6-22 Land-Use Compatibility as a Function of
the Noise Exposure Forecast (NEF)
Land use
NEF
<24 24–30 30–40 >40
Residential S S Qa U
Commercial; industrial S S S U
Hotels, offices, public buildings S S Qb U
Schools, hospitals, churches S Qb U U
Theaters, auditoriums Qc Qb U U
S ј satisfactory; Q ј questionable; U ј unsatisfactory.
aIndividuals may complain, and some may complain vigorously.
New single-family dwelling construction should be avoided.
Noise control features must be included in the building design
for apartment buildings.
bConstruction should be avoided unless a detailed analysis of
noise control requirements is made and the building design
contains the required noise control features.
cA detailed noise analysis is required for any auditorium where
music is to be played.
Source: HUD (1971).
TABLE 6-23 HUD Site Acceptability Categories as Related to Airport Noise
Category Location of the site from the runway center point
Clearly acceptable Outside the NEF-30 controur, at a distance equal to
or greater than the distance between the NEF-30
and NEF-40 contours
Normally acceptable Outside the NEF-30 contour, at a distance less than
the distance between the NEF-30 and NEF-40
contours
Normally acceptable Between the NEF-30 and NEF-40 contours
Clearly unacceptable Within the NEF-40 contour
Source: HUD (1971).
Copyright © 2003 Marcel Dekker, Inc.
ical values of the dimensions L and W are given in Table 6-24. The number
of ‘‘effective’’ flights considers the weighting of noise due to the nighttime
flights:
NEF ј ND ю 16:67NN (6-18)
The application of this approximate procedure is illustrated in the following
example.
It has been observed (Beranek, 1971, p. 583) that the simplified or
approximate procedure is conservative; i.e., the NEF contours according
to the approximate method are larger than those determined through a
more detailed analysis. For this reason, the simplified approach should be
260 Chapter 6
FIGURE 6-4 Description of dimensions used to determine the approximate location
of the NEF-30 and NEF-40 contours. (From HUD, 1971.)
TABLE 6-24 Dimensions for NEF Contour
Approximation
Effective number
of flights, NEF
a
NEF-30 NEF-40
W L W L
0–50 1000 ft 1 mile 0 0
(305 m) (1.6 km)
50–500 0.5 mile 3 miles 1000 ft 1 mile
(0.8 km) (4.8 km) (305 m) (1.6 km)
500–1,300 1.5 mile 6 miles 2000 ft 2.5 miles
(2.4 km) (9.7 km) (610 m) (4.0 km)
>1,300 2 miles 10 miles 3000 ft 4 miles
(3.2 km) (16.1 km) (915 m) (6.4 km)
aThe effective number of flights NEF ј ND ю 16:67NN
Source: HUD (1971).
Copyright © 2003 Marcel Dekker, Inc.
used only for preliminary planning, and the detailed analysis should be
utilized for more detailed planning purposes (Schultz, 1970).
Example 6-10. A small airport has two main runways: (a) an east–west
runway, which is 3 miles (4.83 km) long, and (b) a north–south runway,
which is 2 miles (3.22 km) long. The runways cross at a distance of 0.75
miles (1.21 km) from the west end of the east–west runway and 0.75 miles
(1.21 km) from the south end of the north–south runway, as shown in Fig.
6-5. There are 90 daytime flights (takeoffs plus landings) and 12 nighttime
flights during each 24-hour period. Determine the location of the NEF-30
Acoustic Criteria 261
FIGURE 6-5 Diagram for Example 6-10.
Copyright © 2003 Marcel Dekker, Inc.
and NEF-40 contours, using the approximate method. Also, determine the
limit for the HUD clearly acceptable category for land use.
The equivalent number of flights is found from Eq. (6-18):
NEF ј 90юр16:67Юр12Ю ј 90ю200 ј 290 flights
The dimensions for the NEF contours are found from Table 6-24:
NEF-40: L ј 1 mile (1.6 km) andW ј 1000 ft (305 m)
NEF-30: L ј 3 miles (4.8 km) andW ј 0:5 mile (0.8 km)
These contours are shown in Fig. 6-5.
The limiting line for the HUD ‘‘clearly acceptable’’ category is found.
The difference between the NEF-30 and NEF-40 contours is as follows:
_L ј 3 _ 1 ј 2miles р3:2kmЮ
_W ј 2640 _ 1000 ј 1640 ft ј 0:311 mile р0:500 kmЮ
The dimensions of the limiting line (measured from the runway) are as
follows:
L ј 3 ю 2 ј 5 miles р8:0kmЮ
W ј 0:50 ю 0:311 ј 0:811 miles ј 4280 ft р1:30kmЮ
Популярные книги
- Старинные занимательные задачи
- Медоносные растения
- Algebratic geometry
- Workbook in Higher Algebra
- Математика Древнего Китая
- Finite element analysis
- Mathematics and art
- Fields and galois theory
- Пчеловодство
- Black Holes
Популярные статьи
- Higher-Order Finite Element Methods
- Электровакуумные приборы
- Riemann zeta functionS
- Универсальная открытая архитектурно-строительная система зданий серии Б1.020.1-71
- Complex Analysis 2002-2003
- Пример расчета прочности елементов, стыков и узлов несущего каркаса здания
- Составы, вещества и материалы для огнезащитыметаллических консрукций и изделий
- CMOS Technology
- Рекомендации по расчету и конструированию сборных железобетонных колонн каркасов зданий серии Б1.020.1-7 с плоскими стыками ВИНСТ
- Советы старого пчеловода