radiation of sound waves from a semi-infinite rigid duct
TRANSCRIPT
ยฉ2017 Published in 5th International Symposium on Innovative Technologies in Engineering and Science 29-30 September 2017 (ISITES2017 Baku - Azerbaijan)
*Corresponding author: Address: Faculty of Arts and Sciences, Department of Applied Mathematics, Marmara
University, 34722, Istanbul, TURKEY. E-mail address: [email protected], Phone:+902163451186
Radiation of Sound Waves from a Semi-Infinite Rigid Duct
by Local Outer Lining
*1Burhan Tiryakioglu and 2Ahmet Demir
*1Faculty of Arts and Sciences, Department of Applied Mathematics, Marmara University, Turkey 2Faculty of Engineering, Department of Mechatronics Engineering, Karabuk University, Turkey
Abstract Radiation of sound waves from a semi-infinite rigid duct by local outer lining is investigated
rigorously by the Wiener-Hopf technique. Through the application of Fourier-transform technique in
conjunction with the Mode-Matching method, the radiation problem is described by a modified
Wiener-Hopf equation of the third kind and then solved approximately. The solution involves a set of
infinitely many expansion coefficients satisfying an infinite system of linear algebraic equations.
Numerical solution of this system is obtained for various values of the parameters of the problem and
their effects on the radiation phenomenon are presented.
Key words: Wiener-Hopf technique, Fourier transform, diffraction, duct
1. Introduction
As is well known, the propagation of sound in cylindrical ducts is a major problem in noise
pollution. Accordingly, there have been a number of studies on radiation and propagation in
ducts.
By using the Wiener-Hopf technique which is the efficient method for diffraction/radiation
problems, the radiation of sound from a semi-infinite rigid pipe has been considered by Levine
and Schwinger [1]. One of the effective methods of reducing unwanted noise which has been
found empirically to be very successful is to create large additional sound absorption by lining
the duct with an acoustically absorbent material. Rawlins who showed the effectiveness of this
method, considered the radiation of sound from an unflanged rigid cylindrical duct with an
acoustically absorbing internal surface [2]. Demir and Buyukaksoy solved same problem with
partial linig [3]. They analyzed the effects of the length of internal surface impedance, pipe radius
etc. with graphically for various values of the parameters.
In the present work, a rigorous approximate solution for the problem of sound waves from a
semi-infinite rigid duct by local outer lining, is presented. This is similar to that considered by
Demir and Buyukaksoy [3] which consists of partial internal impedance loading by a semi-
infinite circular cylindrical pipe. In our work, as in the above study, hybrid method was applied.
By stating the total field in duct region in terms of normal waveguide modes (Diniโs series)
and using the Fourier Transform elsewhere, the related boundary value problem is formulated as
a Modified Wiener-Hopf equation of the third kind whose formal solution involves branch-cut
integrals with unknown integrands and infinitely many unknown expansion coefficients
satisfying an infinite system of linear algebraic equations. Some computational results illustrating
B. TIRYAKIOGLU et al./ ISITES2017 Baku - Azerbaijan 1503
the effects of external surface impedance, duct radius etc. on the radiation phenomenon are
presented.
A time factor ๐โ๐๐๐ก with ๐ being the angular frequency is assumed and suppressed
throughout the paper.
2. Analysis
2.1. Formulation of the Problem
The geometry of the problem is sketched in Fig. 1. This geometry consists of a semi-infinite rigid
duct with partial external lining. Duct walls are assumed to be infinitely thin, and they defined by
{๐ = ๐, ๐ง โ (โโ, ๐)}. The part ๐ = ๐, ๐ง โ (0, ๐) of its outer surface is assumed to be treated by an
acoustically absorbent lining which is denoted by ๐ฝ, while the other parts of the duct are assumed
to be rigid.
Figure 1. Geometry of the problem
From the symmetry of the geometry of the problem and of the incident field, the total field
everywhere will be independent of ๐.
The incident sound wave propagating along the positive z direction and is defined by
๐ข๐ = ๐๐๐๐ง (1)
where ๐ = ๐/๐ denotes the wave number. For the sake of analytical convenience, the total field
can be written in different regions as:
๐ข๐(๐, ๐ง) = {
๐ขโ(๐, ๐ง)
๐ข2(๐, ๐ง)
๐ข3(๐, ๐ง) + ๐ข๐
, , ,
๐ > ๐๐ < ๐๐ < ๐
, ๐ง โ (โโ, โ) , ๐ง โ (๐, โ)
, ๐ง โ (โโ, ๐) (2)
where ๐ข๐ is the incident field as given by (1) and the fields ๐ข๐(๐, ๐ง), ๐ = 1,2,3 which satisfy the
Helmholtz equation,
B. TIRYAKIOGLU et al./ ISITES2017 Baku - Azerbaijan 1504
[1
๐
โ
โ๐(๐
โ
โ๐) +
โ2
โz2+ k2] ๐ขj(๐, ๐ง) = 0 , ๐ = 1,2,3 (3)
is to be determined with the help of the following boundary and continuity relations:
โ
โฯ๐ข1(๐, ๐ง) = 0 , ๐ง < 0 ,
โ
โฯ๐ข3(๐, ๐ง) = 0 , ๐ง < ๐ (4๐, ๐)
(๐๐๐ฝ +โ
โฯ) ๐ข1(๐, ๐ง) = 0 , 0 < ๐ง < ๐ (5)
โ
โฯ๐ข1(๐, ๐ง) โ
โ
โฯ๐ข2(๐, ๐ง) = 0 , ๐ง > ๐ , ๐ข1(๐, ๐ง) โ ๐ข2(๐, ๐ง) = 0 , ๐ง > ๐ (6๐, ๐)
โ
โz๐ข2(ฯ, ๐) โ
โ
โz๐ข3(ฯ, ๐) = ๐๐๐๐๐๐ , ฯ < ๐ , ๐ข2(ฯ, ๐) โ ๐ข3(ฯ, ๐) = ๐๐๐๐ , ฯ < ๐ (7๐, ๐)
2.2. Derivation of the Modified Wiener-Hopf Equation
For ๐ > ๐, ๐ขโ(๐, ๐ง) satisfies the Helmholtz equation for ๐ง โ (โโ,โ). Multiplying (3) by ๐๐๐ผ๐ง
with ๐ผ being the Fourier transform variable and integrating the resultant equation with respect to
๐ง from โโ to โ, we obtain
[1
๐
โ
โ๐(๐
โ
โ๐) +
โ2
โz2+ k2] ๐น(๐, ๐ผ) = 0 , ๐ง โ (โโ, โ) (8)
with
๐น(๐, ๐ผ) = โซ ๐ข1(๐, ๐ง)๐๐๐ผ๐ง
โ
โโ
๐๐ง = ๐นโ(๐, ๐ผ) + ๐น1(๐, ๐ผ) + ๐๐๐ผ๐๐น+(๐, ๐ผ) (9)
where
๐นโ(๐, ๐ผ) = โซ ๐ข1(๐, ๐ง)๐๐๐ผ๐ง
0
โโ
๐๐ง , ๐น+(๐, ๐ผ) = โซ ๐ข1(๐, ๐ง)๐๐๐ผ(๐งโ๐)
โ
๐
๐๐ง (10๐, ๐)
๐น1(๐, ๐ผ) = โซ ๐ข1(๐, ๐ง)๐๐๐ผ๐ง
๐
0
๐๐ง (10๐)
here ๐น+(๐, ๐ผ) and ๐นโ(๐, ๐ผ) are analytic functions on upper region ๐ผ๐๐ผ > ๐ผ๐(โ๐) and on lower
region ๐ผ๐๐ผ < ๐ผ๐๐ of the complex ๐ผ-plane, respectively, while ๐น1(๐, ๐ผ) is an entire function.
The general solution of (8) satisfying the radiation condition for ๐ > ๐ reads
B. TIRYAKIOGLU et al./ ISITES2017 Baku - Azerbaijan 1505
๐นโ(๐, ๐ผ) + ๐น1(๐, ๐ผ) + ๐๐๐ผ๐๐น+(๐, ๐ผ) = ๐ด(๐ผ)๐ป0(1)(๐พ๐) (11)
where
๐พ = โ๐2 โ ๐ผ2 , ๐พ(0) = ๐ (12)
is the square root function (see Fig. 2) and
๐ป๐(1)(๐ง) = ๐ฝ๐(๐ง) + ๐๐๐(๐ง) (13)
is the Hankel function of the first kind and ๐-th order. ๐ด(๐ผ) in (11) is a spectral coefficient to be
determined.
Figure 2. Branch-cut and integration lines in the complex plane
Consider now the Fourier transform of (4a) and (5), namely
๐นโฬ (๐, ๐ผ) = 0 , ๐๐๐ฝ๐น1(๐, ๐ผ) + ๐น1ฬ(๐, ๐ผ) = 0 (14๐, ๐)
where the dot specifies the derivative with respect to ๐. The differentiation of (11) with respect to
๐ yields
๐นโฬ (๐, ๐ผ) + ๐น1ฬ(๐, ๐ผ) + ๐๐๐ผ๐ ๐น+ฬ (๐, ๐ผ) = โ๐พ๐ด(๐ผ)๐ป1(1)(๐พ๐) (15)
Setting ๐ = ๐ in (15) and using (14a,b), we obtain
๐ด(๐ผ) =๐โ(๐ผ) + ๐๐๐ผ๐๐+(๐ผ)
๐ป(๐ผ) (16)
where
๐ยฑ(๐ผ) = ๐๐๐ฝ๐นยฑ(๐, ๐ผ) + ๐นยฑฬ (๐, ๐ผ) (17)
๐ป(๐ผ) = ๐๐๐ฝ๐ป0(1)(๐พ๐) โ ๐พ๐ป1
(1)(๐พ๐) (18)
B. TIRYAKIOGLU et al./ ISITES2017 Baku - Azerbaijan 1506
The substitution of ๐ด(๐ผ) given in (16) into (11) yields
๐นโ(๐, ๐ผ) + ๐น1(๐, ๐ผ) + ๐๐๐ผ๐๐น+(๐, ๐ผ) = [๐โ(๐ผ) + ๐๐๐ผ๐๐+(๐ผ)]๐ป0
(1)(๐พ๐)
๐ป(๐ผ) (19)
In the region ๐ < ๐, ๐ง > ๐. By taking the half-range Fourier transform of the Helmholtz equation
satisfies by ๐ข2(๐, ๐ง) we get
[1
๐
โ
โ๐(๐
โ
โ๐) +
โ2
โz2+ K2(๐ผ)] ๐บ+(๐, ๐ผ) = ๐(๐) โ ๐๐ผ๐(๐) (20)
where
๐บ+(๐, ๐ผ) = โซ ๐ข2(๐, ๐ง)๐๐๐ผ(๐งโ๐)
โ
๐
๐๐ง (21)
while ๐(๐) and ๐(๐) stand for
๐(๐) =โ
โz๐ข2(๐, ๐) , ๐(๐) = ๐ข2(๐, ๐) (22๐, ๐)
๐บ+(๐, ๐ผ) is regular function in the upper (๐ผ๐๐ผ > ๐ผ๐(โ๐)) half of the complex ๐ผ-plane. The
particular solution of (20) which is bounded and satisfying the impedance boundary condition at
๐ = ๐ can be obtained by the Greenโs function technique. The Greenโs function related to (20)
satisfies the Helmholtz equation.
[1
๐
โ
โ๐(๐
โ
โ๐) + K2(๐ผ)] ฦ(๐, ๐ก, ๐ผ) = 0 , ๐ โ ๐ก , ๐, ๐ก โ (0, ๐) (23)
the solution is
ฦ(๐, ๐ก, ๐ผ) =1
๐ฝ(๐ผ)๐(๐, ๐ก, ๐ผ) (24๐)
with
๐(๐, ๐ก, ๐ผ) =๐
2{
๐ฝ0(๐พ๐)[๐ฝ(๐ผ)๐0(๐พ๐ก) โ ๐(๐ผ)๐ฝ0(๐พ๐ก)] , 0 โค ๐ โค ๐ก
๐ฝ0(๐พ๐ก)[๐ฝ(๐ผ)๐0(๐พ๐) โ ๐(๐ผ)๐ฝ0(๐พ๐)] , ๐ก โค ๐ โค ๐ (24๐)
where
๐ฝ(๐ผ) = ๐๐๐ฝ๐ฝ0(๐พ๐) โ ๐พ๐ฝ1(๐พ๐) (24๐)
๐(๐ผ) = ๐๐๐ฝ๐0(๐พ๐) โ ๐พ๐1(๐พ๐) (24๐)
The solution of (20) can now be written as
๐บ+(๐, ๐ผ) =1
๐ฝ(๐ผ)[๐ต(๐ผ)๐ฝ0(๐พ๐) + โซ(๐(๐ก) โ ๐๐ผ๐(๐ก))๐(๐ก, ๐, ๐ผ)
๐
0
๐ก๐๐ก] (25)
B. TIRYAKIOGLU et al./ ISITES2017 Baku - Azerbaijan 1507
In (25), ๐ต(๐ผ) is a spectral coefficient to be determined, while ๐ and ๐ are given by (22a,b).
Combining (6a) and (6b) and using Fourier transform, we can write
๐๐๐ฝ๐บ+(๐, ๐ผ) + ๐บ+ฬ (๐, ๐ผ) = ๐+(๐ผ) (26)
Substituting (25) and its derivative with respect to ๐ in (26), one can obtain ๐ต(๐ผ) = ๐+(๐ผ)
Inserting now ๐ต(๐ผ) into (25), we get
๐บ+(๐, ๐ผ) =1
๐ฝ(๐ผ)[๐+(๐ผ)๐ฝ0(๐พ๐) + โซ(๐(๐ก) โ ๐๐ผ๐(๐ก))๐(๐ก, ๐, ๐ผ)
๐
0
๐ก๐๐ก] (27)
The left hand side of (27) is regular in the upper half plane. The regularity of the right hand side
may be violated by the presence of simple poles occurring at the zeros of ๐ฝ(๐ผ) lying in the upper
half plane, namely at ๐ผ = ๐ผ๐, ๐ = 1,2, โฆ
๐๐๐๐ฝ๐ฝ0(๐พ๐) โ ๐พ๐๐ฝ1(๐พ๐) = 0 , ๐ผ๐ = โ๐2 โ (๐พ๐
๐)
2
, ๐ผ๐(๐ผ๐) โฅ ๐ผ๐๐ (28)
We can eliminate these poles by imposing that their residues are zero. This gives
๐+(๐ผ๐) =๐
2๐ฝ0(๐พ๐)[1 โ (๐ฝ๐๐ ๐พ๐โ )2][๐๐ โ ๐๐ผ๐๐๐] (29)
with
[๐๐
๐๐] =
2
๐2๐ฝ02(๐พ๐)[1 โ (๐ฝ๐๐ ๐พ๐โ )2]
โซ [๐(๐ก)
๐(๐ก)] ๐ฝ0 (
๐พ๐
๐๐ก) ๐ก๐๐ก
๐
0
(30๐)
Owing to (30a), ๐(๐) and ๐(๐) can be expanded into Dini series as follows;
[๐(๐)
๐(๐)] = โ [
๐๐
๐๐] ๐ฝ0 (
๐พ๐
๐๐)
โ
๐=1
(30๐)
Using the continuity relation (6b) and combining (19) with (27), we get the following Modified
Wiener-Hopf Equation (MWHE) of the third kind.
๐
2๐นโ(๐, ๐ผ)๐(๐ผ) +
๐๐๐ผ๐๐+(๐ผ)
๐(๐ผ)โ
๐
2๐น1(๐, ๐ผ) = ๐๐๐ผ๐
๐
2โ
๐ฝ0(๐พ๐)
๐ผ๐2 โ ๐ผ2
โ
๐=1
[๐๐ โ ๐๐ผ๐๐] (31๐)
where
๐(๐ผ) = ๐๐๐ฝ(๐ผ)๐ป(๐ผ) , ๐(๐ผ) =๐พ๐ป1
(1)(๐พ๐)
๐ป(๐ผ) (31๐, ๐)
B. TIRYAKIOGLU et al./ ISITES2017 Baku - Azerbaijan 1508
2.3. Approximate Solution of the Modified Wiener-Hopf Equation
By using the factorization and decomposition procedures, together with the Liouville theorem,
the modified Wiener-Hopf equation in (31a) can be reduced to the following system of Fredholm
integral equations of the second kind:
๐+(๐ผ)
๐+(๐ผ)= โ
1
2๐๐
๐
2โซ
๐โ(๐)๐(๐)๐โ๐๐๐๐นโ(๐, ๐)
(๐ โ ๐ผ)๐๐
๐ฟ+
+1
2๐๐
๐
2โซ
๐โ(๐)
(๐ โ ๐ผ)โ
๐ฝ0(๐พ๐)
๐ผ๐2 โ ๐2
โ
๐=1
[๐๐ โ ๐๐๐๐]๐๐ (32๐)
๐ฟ+
๐
2๐นโ(๐, ๐ผ)๐โ(๐ผ) =
1
2๐๐โซ
๐๐๐๐๐+(๐)
๐+(๐)๐(๐)(๐ โ ๐ผ)๐๐
๐ฟโ
โ1
2๐๐
๐
2โซ
๐๐๐๐
๐+(๐)(๐ โ ๐ผ)โ
๐ฝ0(๐พ๐)
๐ผ๐2 โ ๐2
โ
๐=1
[๐๐ โ ๐๐๐๐]๐๐ (32๐)
๐ฟโ
where ๐+(๐ผ), ๐+(๐ผ) and ๐โ(๐ผ), ๐โ(๐ผ) are the split functions, analytic and free of zeros in the
upper and lower halves of the complex ๐ โ plane, respectively, resulting from the Wiener-Hopf
factorization of ๐(๐ผ) and ๐(๐ผ) which are given by (31b) and (31c), in the following form:
๐(๐ผ) = ๐+(๐ผ)๐โ(๐ผ) , ๐(๐ผ) = ๐+(๐ผ)๐โ(๐ผ) (33๐, ๐)
Here the explicit forms for ๐+(๐ผ), ๐โ(๐ผ) and ๐+(๐ผ), ๐โ(๐ผ) can be obtained as is done in [4].
For large argument, the coupled system of Fredholm integral equations of the second kind in
(32a,b), is susceptible to a treatment by iterations. Now, the approximate solution of the MWHE
reads:
๐+(๐ผ)
๐+(๐ผ)โ
๐
2โ
๐ฝ0(๐พ๐)[๐๐ + ๐๐ผ๐๐๐]๐+(๐ผ๐)
2๐ผ๐(๐ผ + ๐ผ๐)+
๐
2
โ
๐=1
โ๐ฝ0(๐พ๐)[๐๐ โ ๐๐ผ๐๐๐]๐๐๐ผ๐๐
2๐ผ๐๐+(๐ผ๐)
โ
๐=1
๐ผ1(๐ผ) (34๐)
๐นโ(๐, ๐ผ)๐โ(๐ผ) โ โ โ๐ฝ0(๐พ๐)[๐๐ โ ๐๐ผ๐๐๐]๐๐๐ผ๐๐
2๐ผ๐๐+(๐ผ๐)(๐ผ โ ๐ผ๐)+
โ
๐=1
โ๐ฝ0(๐พ๐)[๐๐ + ๐๐ผ๐๐๐]๐+(๐ผ๐)
2๐ผ๐
โ
๐=1
๐ผ2(๐ผ)
(34๐) with
๐ผ1(๐ผ) =1
2๐๐โซ
๐โ(๐)๐(๐)๐โ๐๐๐
(๐ โ ๐)(๐ โ ๐ผ๐)๐โ(๐)๐๐
๐ฟ+
, ๐ผ2(๐ผ) = 1
2๐๐โซ
๐+(๐)๐๐๐๐
๐+(๐)๐(๐)(๐ โ ๐)(๐ + ๐ผ๐)๐๐
๐ฟโ
(35๐, ๐)
B. TIRYAKIOGLU et al./ ISITES2017 Baku - Azerbaijan 1509
The integral given by (35a,b) can be obtained numerically. First the integration line ๐ฟยฑ can be
deformed onto the branch-cut, then the integrals can be evaluated by the help of Cauchy theorem.
2.4. Reduction to an Infinite System of Linear Algebraic Equations
In the region ๐ < ๐, ๐ง < ๐, ๐ขโ(๐, ๐ง) can be expressed as
๐ขโ(๐, ๐ง) = โ ๐๐๐โ๐๐๐๐ง
โ
๐=0
๐ฝ0 (๐ฝ๐
๐๐) (36๐)
with
๐ฝ1(๐ฝ๐) = 0 , ๐๐ = โ๐2 โ (๐ฝ๐
๐)
2
, ๐0 = ๐ (36๐)
From the continuity relations (7a,b) and using (30b).
โ ๐๐๐ฝ0 (๐พ๐
๐๐) =
โ
๐=1
โ ๐ โ ๐๐๐๐๐โ๐๐๐๐
โ
๐=0
๐ฝ0 (๐ฝ๐
๐๐) + ๐๐๐๐๐๐ (37๐)
โ ๐๐๐ฝ0 (๐พ๐
๐๐) =
โ
๐=1
โ ๐๐๐โ๐๐๐๐
โ
๐=0
๐ฝ0 (๐ฝ๐
๐๐) + ๐๐๐๐ (37๐)
Then multiply both sides of (37a,b) by ๐๐ฝ0 (๐ฝ๐
๐๐) and integrate from ๐ = 0 to ๐ = ๐. We get
โ๐ฝ0(๐พ๐)
๐พ๐2
โ
๐=1
[๐๐ + ๐๐๐๐] =๐๐๐๐
๐๐ฝ , ๐ = 0 (38๐)
2๐๐๐ฝ
๐๐๐ฝ0(๐ฝ๐)โ
๐ฝ0(๐พ๐)
๐พ๐2 โ ๐ฝ๐
2
โ
๐=1
[๐๐ + ๐๐๐๐๐] = 0 , ๐ = 1,2, โฆ (38๐)
By substituting ๐ผ = ๐ผ1, ๐ผ2, ๐ผ3, โฆ in (34a) and using (29) we obtain
๐ฝ0(๐พ๐)[1 โ (๐ฝ๐๐ ๐พ๐โ )2][๐๐ โ ๐๐ผ๐๐๐]
๐+(๐ผ๐)= โ
๐ฝ0(๐พ๐)[๐๐ + ๐๐ผ๐๐๐]๐+(๐ผ๐)
2๐ผ๐(๐ผ๐ + ๐ผ๐)
โ
๐=1
+ โ๐ฝ0(๐พ๐)[๐๐ โ ๐๐ผ๐๐๐]๐๐๐ผ๐๐
2๐ผ๐๐+(๐ผ๐)
โ
๐=1
๐ผ1(๐ผ๐) (39)
(38a,b) and (39) are the required linear system of algebraic equations which permits us to
determine ๐๐ and ๐๐. The coefficient ๐๐ can be found from ๐๐ or ๐๐. All the numerical results
will be derived by truncating the infinite series and the infinite systems of linear algebraic
equations after first ๐ term. It was seen that the amplitude of the radiated field becomes
insensitive to the increase of the truncation after ๐ = 20.
B. TIRYAKIOGLU et al./ ISITES2017 Baku - Azerbaijan 1510
2.5. Analysis of the Field
The total field in the region ๐ > ๐ can be obtained by taking the inverse Fourier transform of
๐น(๐, ๐ผ). From (11) and (16), one can write
๐ข1(๐, ๐ง) =1
2๐โซ ๐๐๐ฝ๐นโ(๐, ๐ผ)
๐ป0(1)(๐พ๐)
๐ป(๐ผ)๐
๐โ๐๐ผ๐ง๐๐ผ +1
2๐โซ ๐+(๐ผ)
๐ป0(1)(๐พ๐)
๐ป(๐ผ)๐โ๐๐ผ(๐งโ๐)๐๐ผ
๐
(40๐)
where ๐ is a straight line parallel to the real ๐ผ-axis, lying in the strip ๐ผ๐(โ๐) < ๐ผ๐๐ผ < ๐ผ๐๐.
Utilizing the asymptotic expansion of Hankel function and using the saddle point technique, we
get
๐ข1(๐, ๐ง)~๐
๐๐[๐๐๐ฝ๐นโ(๐, โ๐๐๐๐ ๐1)
H(โ๐๐๐๐ ๐1)
๐๐๐๐1
๐๐1+
๐+(โ๐ cos ฮธ2)
H(โ๐๐๐๐ ๐2)
๐๐๐๐2
๐๐2] (40๐)
where ๐1, ฮธ1 and ๐2, ฮธ2 are the spherical coordinates defined by
๐ = ๐1๐ ๐๐ฮธ1 , z = ๐1๐๐๐ ฮธ1 (41a)
and
๐ = ๐2๐ ๐๐ฮธ2 , z โ l = ๐2๐๐๐ ฮธ2 (41b)
3. Numerical Results
In this section, some graphics displaying the effects of the radius of the pipe, the external lining
etc. on the radiation phenomenon are presented. The far field values are plotted at a distance 46 m
away from the duct edge. Figure 3 shows the variation of the amplitude of the radiated field
against the observation angle for different values of the impedance. From Figure 4, it is observed
that the radiated field increases with increasing duct radius, as expected.
Figure 3. 20๐๐๐|๐ข1| versus the observation angle for
different values of the impedance.
Figure 4. 20๐๐๐|๐ข1| versus the observation
angle for different values of the duct radius.
Figure 5 shows the variation the modules of reflection coefficient |๐0| with respect to frequency ๐
for different positive values of the lining impedance ๐ฝ. Finally Figure 6 displays the variation of
B. TIRYAKIOGLU et al./ ISITES2017 Baku - Azerbaijan 1511
the amplitude of the radiated field versus ๐.
Figure 5. Variation of the reflection coefficient
|๐0| versus frequency ๐.
Figure 6. 20๐๐๐|๐ข1| versus ๐.
4. Conclusions
The radiation of sound waves from a semi-infinite rigid duct whose outer surface is treated by an
acoustically absorbing material of finite length, has been investigated by using the mode-
matching method in conjunction with the Wiener-Hopf technique. This problem is more
complicated due to partial lining of the external surface. To overcome the additional difficulty
caused by the finite impedance discontinuity, the problem was first reduced to a system of
Fredholm integral equations of the second kind and then solved approximately by iterations. The
solution involves two systems of linear algebraic equations involving two sets of infinitely many
unknown expansion coefficient. A numerical solution to these systems has obtained for various
values of the parameters such as radius ๐, outer partial impedance ๐ฝ and wave number ๐.
Acknowledgement
The first author would like to thank TUBITAK (The Scientific and Technological Research
Council of Turkey) for continued support.
References
[1] Levine H, Schwinger J. On the radiation of sound from an unflanged circular pipe. Physical
Review, 73, p. 383-406, 1948.
[2] Rawlins AD. Radiation of sound from an unflanged rigid cylindrical duct with an acoustically
absorbing internal surface. Proc. Roy. Soc. Lond. A. 361, p. 65-91, 1978.
[3] Demir A, Buyukaksoy A. Radiation of plane sound waves by a rigid circular cylindrical pipe
with a partial internal impedance loading. Acta Acustica with U. A. 89, p. 578-585, 2003.
[4] Buyukaksoy A and Polat B. Diffraction of acoustic waves by a semi-infinite cylindrical
impedance pipe of certain wall thickness. J. Engin. Math. 33, 333-352, 1998.