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TM plane-wave scattering from nite
rectangular grooves in a conducting plane
using overlapping T-block method
Yong H. Cho
School of Information and Communication Engineering
Mokwon University
800 Doan-dong, Seo-gu, Daejeon, 302-729, Republic of Korea
Phone: +82-42-829-7675 Fax: +82-42-825-5449
Email: yhcho@mokwon.ac.kr
October 24, 2005 DRAFT
2
Abstract
TM plane-wave scattering from nite rectangular grooves in a conducting plane is systematically
analyzed with the overlapping T-block method. Multiple rectangular grooves are divided into several
overlapping T-blocks to obtain the fast CPU time, simple applicability, and wide versatility. The eld
representations within T-blocks are expressed using the Green's function relation and mode-matching
method. The scattered elds are obtained in simple closed forms including a fast-convergent integral.
I. Introduction
TM plane-wave scattering from nite rectangular grooves in a conducting plane is a
fundamental problem and has been extensively studied 1-11]. In 1], the integral equation
for a narrow gap is derived and solved with the moment method using pulse basis and point
matching functions. A third order GIBC (Generalized Impedance Boundary Condition) is
applied to the scattering from a two-dimensional groove, which is solved with the conjugate
gradient fast Fourier transform method 2]. The quasi-static integral equation for a narrow
rectangular groove is also obtained in 3]. In 4], the nite element method and generalized
network formulation is applied to get the admittance matrix of a two-dimensional cavity.
The Fourier transform technique is utilized to derive a fast-convergent series solution 5,
6]. To analyze electromagnetic scattering of a wide groove, a hybrid FE-FMM (Finite
Element-Fast Multipole Method) is proposed in 7]. The superdirective radiation from
nite gratings of rectangular grooves is investigated using the modal approach 8]. Some
techniques for the problems of three-dimensional gratings within rectangular or circular
waveguides are proposed in 12-14].
In the present work, we introduce a novel approach based on the overlapping T-block
method for the scattering from nite rectangular grooves in a conducting plane. The dis-
persion analyses 15, 16] of overlapping T-blocks are extended to the scattering analysis
of nite rectangular grooves. The nite rectangular grooves are divided into several over-
lapping T-blocks. The Hz elds within T-blocks are obtained using the Green's function
relation 15] and mode-matching technique. A new formulation of a T-block for the rect-
angular groove is introduced, which is di erent from those in 15, 16]. The main advantage
of the overlapping T-block method is that scattering relations of nite rectangular grooves
are obtained as simple closed forms without the need of the residue calculus 5, 6] and
October 24, 2005 DRAFT
3
PEC
a2
d
e1
),( yxH i
z
Region(II)
Region(I)
x
y
z
C2
C3
e2
C1
oi
Fig. 1. Geometry of a rectangular groove.
the integral equation technique 1-4]. Our dominant-mode solution for the normal inci-
dence is quite accurate and useful for numerical evaluation, thus con rming the fast CPU
time, simple applicability, and wide versatility. The overlapping T-block method allows
us to obtain a simple yet numerically e cient series solution including a fast-convergent
integral.
II. Field Analysis of a Single Groove
Consider a rectangular groove with the TM plane-wave incidence shown in Fig. 1. The
time-factor e i!t is suppressed throughout. The incident and re ected Hz elds are shown
as, respectively,
Hi
z(x;y) = exp ik2(sin ix cos iy)] (1)
Hr
z(x;y) = exp ik2(sin ix + cos iy)] (2)
where k2 = !p 2 2 = 2 = 2 and i is an incident angle of the TM plane-wave. In regions
(I) ( d < y < 0) and (II) (y > 0), the Hz components are
HI
z(x;y) =
1X
m=0
qm cosam(x + a)cos m(y + d)
h
u(x + a) u(x a)
i
(3)
HII
z (x;y) =
1X
m=0
qm
2
1
m sin( md)
h
Hm(x;y) + RH
m(x;y)
i
(4)
where am = m =(2a), m =
q
k2
1 a2
m, k1 = !p 1 1 = 2 = 1, and u( ) is a unit step
function. By utilizing the subregions in Fig. 2 and the Green's function relation 15, 16],
October 24, 2005 DRAFT
4
PEC
a2
d
e1
Region(II)
Region(I)
x
y
z
e2n^ n^
(a) Subregion for Hm(x;y)
PEC a2
Region(II)
x
y
z
e2
(b) Subregion for RH
m(x;y)
Fig. 2. Subregions of region (II).
we obtain
Hm(x;y) = ei my
i m
cosam(x + a)
h
u(x + a) u(x a)
i
(5)
RH
m(x;y) = k2
Z 1
0
(2v i)cos( y)
2 a2
mh
( 1)msgn(x a)ei jx aj sgn(x + a)ei jx+aj
i
dv (6)
where m =
q
k2
2 a2
m, = k2v(v i), =
q
k2
2 2, and sgn( ) = 2u( ) 1. To facilitate
the numerical integration of (6) for large y, (5) and (6) reduce to a simpli ed one as
Hm(x;y) + RH
m(x;y) = i
2
Z a
a
H(1)
0 (k2
q
(x x0)2 + y2)cosam(x0 + a) dx0 (7)
where H(1)
0 ( ) is the zeroth order Hankel function of the rst kind. The total magnetic
eld is, therefore, given as
TH(x;y) = HI
z(x;y) + HII
z (x;y) : (8)
October 24, 2005 DRAFT
5
Multiplying the Hz eld continuity at y = 0 by cosal(x + a) and integrating over a <
x < a 15, 16] gives
1X
m=0
qmIH(0;a) = 2Gl(k2 sin i;a) (9)
where
IH(0;a) =
Z a
a
h
HI
z(x0;0) HII
z (x0;0)
i
cosal(x0 + a) dx0 (10)
Gl( ;a) = i e i a ( 1)lei a]
2 a2
l
: (11)
By using (7) and integration by substitution, (10) can be transformed to a nite integral
as
IH(0;a) = a m ml cos( md) + 2
1
m sin( md)
Z 2a
2a
H(1)
0 (k2jx0j)Rml(x0) dx0 (12)
where 0 = 2, m = 1 (m = 1;2; ), ml is the Kronecker delta,
Rml(x0) =
Z min(a; x0
+a)
max( a; x0
a)
cosam(x + a)cosal(x x0 + a) dx (13)
and max(x;y) and min(x;y) in (13) denote the greater and lesser of x or y, respectively.
Note that (13) is similar to the correlation matrix in 17, 18]. When =
px2 + y2 ! 1,
(4) becomes
HII
z ( ; ) ei(k2 + =4)
p2 k2
2
1
1X
m=0
qm m sin( md)Gm( k2 sin ;a) (14)
where = tan 1(x=y).
III. Field Analysis of Multiple Grooves
It is possible to apply the overlapping T-block approach to the geometry of multiple
rectangular grooves shown in Fig. 3. We rst divide the multiple grooves in Fig. 3 into
several overlapping T-blocks as shown in Fig. 4. The superposition procedures are also
utilized in 15, 16]. The Hz elds of Fig. 3 are represented as
Hz(x;y) = T(1)
H (x;y) + T(2)
H (x T(2);y) + + T(N)
H (x T(N);y)
=
NX
n=1
T(n)
H (x T(n);y) (15)
October 24, 2005 DRAFT
6
PEC
a2
e1
),( yxH i
z
x
y
z
e2
e1 e1
(1)
a2
(2)
d
(1)
a2
d
...
d
(2)
...T
(2)
T
(1)
(2)
( )N
( )N
( )N
( )N
Fig. 3. Geometry of multiple rectangular grooves.
a2
e1
e2
e1 e1
(1)
a2
(2)
d
(1)
a2
d(1)
(2)
...
+
e2
d
(2)
+
e2
( )N
( )N
( )Nx'
y'
z x'
y'
z x'
y'
z
T (x',y')
(1)
T (x',y')
(2)
T (x',y')
(N)
...
Fig. 4. Superposition of overlapping T-blocks.
where T(1) = 0 and N is the number of grooves. By using (9), the scattering relations
for multiple rectangular grooves in Fig. 3 can be easily obtained 15, 16]. When =
px2 + y2 ! 1, (4) becomes
HII
z ( ; ) ei(k2 + =4)
p2 k2
NX
n=1
2
(n)
1
e ik2 sin T(n)
1X
m=0
q(n)
m
(n)
m sin( (n)
m d(n))Gm( k2 sin ;a(n)) : (16)
IV. Numerical Computations
To understand the scattering characteristics of nite rectangular grooves, we de ne a
backscattered echowidth as
= lim!12 HII
z ( ; )
Hi
z( ; i)
2
: (17)
Fig. 5 shows the behaviors of a normalized backscattered echowidth versus a normalized
groove width for the normal incidence ( i = 0). Note that 0 in Fig. 5 denotes a free-
October 24, 2005 DRAFT
7
0 0.4 0.8 1.2 1.6 2
−20
−10
0
10
20
Normalized groove width, 2a / λ0
Backscatteredechowdith,σ/λ0
[dB]
ε
1
= 2ε
0
ε1
= 4ε0
m = 0
m = 2
m = 4
m = 6
[3]
Fig. 5. Behaviors of a normalized backscattered echowidth, = 0 versus a normalized groove width, 2a= 0
for i = 0, d = 0:2 0, and 1 = 2 = 0.
space wavelength. When m = 0;2;4;6, our series solutions agree well with the quasi-
static solution 3]. Our computational experience indicates that a dominant-mode solution
(m = 0) for the normal incidence is almost identical to a more accurate solution including
six higher-modes (m = 6). When 2a= 0 = 1, the computational times (Pentium(R) CPU
1.7 GHz, RAM 256 MB) for m = 0;2;4;6 are 78 s, 750 s, 2.7 ms, 6.7 ms, respectively.
The peaks of backscattered echowidths are observed at 2a= 0 = 0.97, 1.95 for 1 = 2 0
and 2a= 0 = 0.60, 1.19, 1.79 for 1 = 4 0, respectively. The peaks in Fig. 5 may come
from the cavity resonance ( md =2) formed by a dielectric- lled groove.
Fig. 6 illustrates the behaviors of a normalized backscattered echowidth versus an
incident angle, i. It is seen that our higher-mode solutions (m = 2;4;6) agree well with
11]. A dominant-mode solution is accurate only near to the normal incidence (0 < i <
5 ).
Fig. 7 shows the behaviors of a normalized radiationpattern versus an observation angle,
for fteen rectangular grooves. Note that the geometry of fteen rectangular grooves
is taken from 8]. Numerical computations are performed with seven modes (m = 6).
The increase in the incident angle, i causes the increase in the mainbeam angle of fteen
October 24, 2005 DRAFT
8
0 10 20 30 40 50 60 70 80 90
−15
−10
−5
0
5
10
15
Incident angle, θ
i
[Degree]
Backscatteredechowidth,σ/λ
0
[dB]
m = 0
m = 2
m = 4
m = 6
[11]
Fig. 6. Behaviors of a normalized backscattered echowidth, = 0 versus an incident angle, i for a =
0:5 m], d = 0:25 m], f = 300 MHz], and 1 = 2 = 0.
−90 −60 −30 0 30 60 90
−25
−20
−15
−10
−5
0
Observation angle, θ [Degree]
Normalizedradiationpattern[dB]
θi
= 0o
θi
= 10o
θi
= 20o
θi
= 30o
Fig. 7. Behaviors of a normalized radiation pattern versus an observation angle, for k1d = 1:57079628,
a = 0:1d, N = 15, T(n)
= 0:9d n=4;7;10;13
, T(n)
= 0:4d n6=4;7;10;13
, and 1 = 2 = 0.
October 24, 2005 DRAFT
9
rectangular grooves. When i < 20 , the 3 dB beamwidth of radiation patterns in Fig. 7
is less than 25 .
V. Conclusions
Scattering analysis of nite rectangular grooves in a conducting plane is analytically
shown using the overlapping T-block method. Simple yet rigorous scattering relations for
nite rectangular grooves are presented and compared with other results. The behaviors
of a backscattered echowidth and a radiation pattern are studied in terms of a normalized
groove width and an incident angle. A dominant-mode solution for the normal incidence
is shown to be accurate and useful for the scattering of nite rectangular grooves.
References
1] T. B. A. Senior, K. Sarabandi, and J. R. Natzke, Scattering by a narrow gap," IEEE Trans. Antennas
Propagat., vol. 38, no. 7, pp. 1102-1110, July 1990.
2] K. Barkeshli and J. L. Volakis, TE scattering by a two-dimensional groove in a ground plane using higher
order boundary conditions," IEEE Trans. Antennas Propagat., vol. 38, no. 9, pp. 1421-1428, Sept. 1990.
3] K. Barkeshli and J. L. Volakis, Scattering from narrow rectangular lled grooves," IEEE Trans. Antennas
Propagat., vol. 39, no. 6, pp. 804-810, June 1991.
4] S.-K. Jeng, Scattering from a cavity-backed slit in a ground plane-TE case," IEEE Trans. Antennas Propagat.,
vol. 38, no. 10, pp. 1523-1529, Oct. 1990.
5] T. J. Park and H. J. Eom, An analysis of transverse electric scattering from a rectangular channel in a
conducting plane," Radio Sci., vol. 28, no. 5, pp. 663-673, Sept.-Oct. 1993.
6] T. J. Park, S. H. Kang, and H. J. Eom, TE scattering from a slit in a thick conducting screen: Revisited,"
IEEE Trans. Antennas Propagat., vol. 42, no. 1, pp. 112-114, Jan. 1994.
7] S. S. Bindiganavale and J. L. Volakis, A hybrid FE-FMM technique for electromagnetic scattering," IEEE
Trans. Antennas Propagat., vol. 45, no. 1, pp. 180-181, Jan. 1997.
8] D. C. Skigin, V. V. Veremey, and R. Mittra, Superdirective radiation from nite gratings of rectangular
grooves," IEEE Trans. Antennas Propagat., vol. 47, no. 2, pp. 376-383, Feb. 1999.
9] Y. Shifman and Y. Leviatan, Scattering by a groove in a conducting plane-A PO-MoM hybrid formulation
and wavelet analysis," IEEE Trans. Antennas Propagat., vol. 49, no. 12, pp. 1807-1811, Dec. 2001.
10] E. Howe and A. Wood, TE solutions of an integral equations method for electromagnetic scattering from a
2-D cavity," IEEE Antennas Wireless Propagat. Lett., vol. 2, pp. 93-96, 2003.
11] T. Van and A. W. Wood, Finite element analysis of electromagnetic scattering from a cavity," IEEE Trans.
Antennas Propagat., vol. 51, no. 1, pp. 130-137, Jan. 2003.
12] I. G. Tigelis, M. Pedrozzi, P. G. Cottis, and J. L. Vomvoridis, Calculation of eigenmodes in a nonperiodic
corrugated waveguide, IEEE Trans. Microwave Theory Tech., vol. 45, no. 2, pp. 236-244, Feb. 1997.
13] G. I. Zaginaylov, A. Hirata, T. Ueda, and T. Shiozawa, Full-wave modal analysis of the rectangular waveguide
grating," IEEE Trans. Plasma Sci., vol. 28, no. 3, pp. 614-620, June 2000.
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10
14] G. P. Anastasiou, G. P. Latsas, I. G. Tigelis, M. Dehler, P. Que elec, and N. F. Dasyras, Calculation of
the electromagnetic waves in nonperiodic corrugated waveguides with dielectric loading," IEEE Trans. Plasma
Sci., vol. 32, no. 3, pp. 1310-1317, June 2004.
15] Y. H. Cho and H. J. Eom, Analysis of a ridge waveguide using overlapping T-blocks," IEEE Trans. Microwave
Theory Tech., vol. 50, no. 10, pp. 2368-2373, Oct. 2002.
16] Y. H. Cho and H. J. Eom, Overlapping T-block analysis of axially grooved rectangular waveguide," Electron.
Lett., vol. 39, no. 24, pp. 1734-1735, Nov. 2003.
17] R. H. MacPhie and A. I. Zaghloul, Radiation from a rectangular waveguide with in nite ange - Exact
solution by the correlation matrix method," IEEE Trans. Antennas Propagat., vol. 28, no. 4, pp. 497-503, July
1980.
18] K. J. Bois, A. D. Benally, and R. Zoughi, Multimode solution for the re ection properties of an open-ended
rectangular waveguide radiating into a dielectric half-space: The forward and inverse problems," IEEE Trans.
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October 24, 2005 DRAFT

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TM plane wave scattering from finite rectangular grooves in a conducting plane using overlapping T-block method

  • 1. 1 TM plane-wave scattering from nite rectangular grooves in a conducting plane using overlapping T-block method Yong H. Cho School of Information and Communication Engineering Mokwon University 800 Doan-dong, Seo-gu, Daejeon, 302-729, Republic of Korea Phone: +82-42-829-7675 Fax: +82-42-825-5449 Email: yhcho@mokwon.ac.kr October 24, 2005 DRAFT
  • 2. 2 Abstract TM plane-wave scattering from nite rectangular grooves in a conducting plane is systematically analyzed with the overlapping T-block method. Multiple rectangular grooves are divided into several overlapping T-blocks to obtain the fast CPU time, simple applicability, and wide versatility. The eld representations within T-blocks are expressed using the Green's function relation and mode-matching method. The scattered elds are obtained in simple closed forms including a fast-convergent integral. I. Introduction TM plane-wave scattering from nite rectangular grooves in a conducting plane is a fundamental problem and has been extensively studied 1-11]. In 1], the integral equation for a narrow gap is derived and solved with the moment method using pulse basis and point matching functions. A third order GIBC (Generalized Impedance Boundary Condition) is applied to the scattering from a two-dimensional groove, which is solved with the conjugate gradient fast Fourier transform method 2]. The quasi-static integral equation for a narrow rectangular groove is also obtained in 3]. In 4], the nite element method and generalized network formulation is applied to get the admittance matrix of a two-dimensional cavity. The Fourier transform technique is utilized to derive a fast-convergent series solution 5, 6]. To analyze electromagnetic scattering of a wide groove, a hybrid FE-FMM (Finite Element-Fast Multipole Method) is proposed in 7]. The superdirective radiation from nite gratings of rectangular grooves is investigated using the modal approach 8]. Some techniques for the problems of three-dimensional gratings within rectangular or circular waveguides are proposed in 12-14]. In the present work, we introduce a novel approach based on the overlapping T-block method for the scattering from nite rectangular grooves in a conducting plane. The dis- persion analyses 15, 16] of overlapping T-blocks are extended to the scattering analysis of nite rectangular grooves. The nite rectangular grooves are divided into several over- lapping T-blocks. The Hz elds within T-blocks are obtained using the Green's function relation 15] and mode-matching technique. A new formulation of a T-block for the rect- angular groove is introduced, which is di erent from those in 15, 16]. The main advantage of the overlapping T-block method is that scattering relations of nite rectangular grooves are obtained as simple closed forms without the need of the residue calculus 5, 6] and October 24, 2005 DRAFT
  • 3. 3 PEC a2 d e1 ),( yxH i z Region(II) Region(I) x y z C2 C3 e2 C1 oi Fig. 1. Geometry of a rectangular groove. the integral equation technique 1-4]. Our dominant-mode solution for the normal inci- dence is quite accurate and useful for numerical evaluation, thus con rming the fast CPU time, simple applicability, and wide versatility. The overlapping T-block method allows us to obtain a simple yet numerically e cient series solution including a fast-convergent integral. II. Field Analysis of a Single Groove Consider a rectangular groove with the TM plane-wave incidence shown in Fig. 1. The time-factor e i!t is suppressed throughout. The incident and re ected Hz elds are shown as, respectively, Hi z(x;y) = exp ik2(sin ix cos iy)] (1) Hr z(x;y) = exp ik2(sin ix + cos iy)] (2) where k2 = !p 2 2 = 2 = 2 and i is an incident angle of the TM plane-wave. In regions (I) ( d < y < 0) and (II) (y > 0), the Hz components are HI z(x;y) = 1X m=0 qm cosam(x + a)cos m(y + d) h u(x + a) u(x a) i (3) HII z (x;y) = 1X m=0 qm 2 1 m sin( md) h Hm(x;y) + RH m(x;y) i (4) where am = m =(2a), m = q k2 1 a2 m, k1 = !p 1 1 = 2 = 1, and u( ) is a unit step function. By utilizing the subregions in Fig. 2 and the Green's function relation 15, 16], October 24, 2005 DRAFT
  • 4. 4 PEC a2 d e1 Region(II) Region(I) x y z e2n^ n^ (a) Subregion for Hm(x;y) PEC a2 Region(II) x y z e2 (b) Subregion for RH m(x;y) Fig. 2. Subregions of region (II). we obtain Hm(x;y) = ei my i m cosam(x + a) h u(x + a) u(x a) i (5) RH m(x;y) = k2 Z 1 0 (2v i)cos( y) 2 a2 mh ( 1)msgn(x a)ei jx aj sgn(x + a)ei jx+aj i dv (6) where m = q k2 2 a2 m, = k2v(v i), = q k2 2 2, and sgn( ) = 2u( ) 1. To facilitate the numerical integration of (6) for large y, (5) and (6) reduce to a simpli ed one as Hm(x;y) + RH m(x;y) = i 2 Z a a H(1) 0 (k2 q (x x0)2 + y2)cosam(x0 + a) dx0 (7) where H(1) 0 ( ) is the zeroth order Hankel function of the rst kind. The total magnetic eld is, therefore, given as TH(x;y) = HI z(x;y) + HII z (x;y) : (8) October 24, 2005 DRAFT
  • 5. 5 Multiplying the Hz eld continuity at y = 0 by cosal(x + a) and integrating over a < x < a 15, 16] gives 1X m=0 qmIH(0;a) = 2Gl(k2 sin i;a) (9) where IH(0;a) = Z a a h HI z(x0;0) HII z (x0;0) i cosal(x0 + a) dx0 (10) Gl( ;a) = i e i a ( 1)lei a] 2 a2 l : (11) By using (7) and integration by substitution, (10) can be transformed to a nite integral as IH(0;a) = a m ml cos( md) + 2 1 m sin( md) Z 2a 2a H(1) 0 (k2jx0j)Rml(x0) dx0 (12) where 0 = 2, m = 1 (m = 1;2; ), ml is the Kronecker delta, Rml(x0) = Z min(a; x0 +a) max( a; x0 a) cosam(x + a)cosal(x x0 + a) dx (13) and max(x;y) and min(x;y) in (13) denote the greater and lesser of x or y, respectively. Note that (13) is similar to the correlation matrix in 17, 18]. When = px2 + y2 ! 1, (4) becomes HII z ( ; ) ei(k2 + =4) p2 k2 2 1 1X m=0 qm m sin( md)Gm( k2 sin ;a) (14) where = tan 1(x=y). III. Field Analysis of Multiple Grooves It is possible to apply the overlapping T-block approach to the geometry of multiple rectangular grooves shown in Fig. 3. We rst divide the multiple grooves in Fig. 3 into several overlapping T-blocks as shown in Fig. 4. The superposition procedures are also utilized in 15, 16]. The Hz elds of Fig. 3 are represented as Hz(x;y) = T(1) H (x;y) + T(2) H (x T(2);y) + + T(N) H (x T(N);y) = NX n=1 T(n) H (x T(n);y) (15) October 24, 2005 DRAFT
  • 6. 6 PEC a2 e1 ),( yxH i z x y z e2 e1 e1 (1) a2 (2) d (1) a2 d ... d (2) ...T (2) T (1) (2) ( )N ( )N ( )N ( )N Fig. 3. Geometry of multiple rectangular grooves. a2 e1 e2 e1 e1 (1) a2 (2) d (1) a2 d(1) (2) ... + e2 d (2) + e2 ( )N ( )N ( )Nx' y' z x' y' z x' y' z T (x',y') (1) T (x',y') (2) T (x',y') (N) ... Fig. 4. Superposition of overlapping T-blocks. where T(1) = 0 and N is the number of grooves. By using (9), the scattering relations for multiple rectangular grooves in Fig. 3 can be easily obtained 15, 16]. When = px2 + y2 ! 1, (4) becomes HII z ( ; ) ei(k2 + =4) p2 k2 NX n=1 2 (n) 1 e ik2 sin T(n) 1X m=0 q(n) m (n) m sin( (n) m d(n))Gm( k2 sin ;a(n)) : (16) IV. Numerical Computations To understand the scattering characteristics of nite rectangular grooves, we de ne a backscattered echowidth as = lim!12 HII z ( ; ) Hi z( ; i) 2 : (17) Fig. 5 shows the behaviors of a normalized backscattered echowidth versus a normalized groove width for the normal incidence ( i = 0). Note that 0 in Fig. 5 denotes a free- October 24, 2005 DRAFT
  • 7. 7 0 0.4 0.8 1.2 1.6 2 −20 −10 0 10 20 Normalized groove width, 2a / λ0 Backscatteredechowdith,σ/λ0 [dB] ε 1 = 2ε 0 ε1 = 4ε0 m = 0 m = 2 m = 4 m = 6 [3] Fig. 5. Behaviors of a normalized backscattered echowidth, = 0 versus a normalized groove width, 2a= 0 for i = 0, d = 0:2 0, and 1 = 2 = 0. space wavelength. When m = 0;2;4;6, our series solutions agree well with the quasi- static solution 3]. Our computational experience indicates that a dominant-mode solution (m = 0) for the normal incidence is almost identical to a more accurate solution including six higher-modes (m = 6). When 2a= 0 = 1, the computational times (Pentium(R) CPU 1.7 GHz, RAM 256 MB) for m = 0;2;4;6 are 78 s, 750 s, 2.7 ms, 6.7 ms, respectively. The peaks of backscattered echowidths are observed at 2a= 0 = 0.97, 1.95 for 1 = 2 0 and 2a= 0 = 0.60, 1.19, 1.79 for 1 = 4 0, respectively. The peaks in Fig. 5 may come from the cavity resonance ( md =2) formed by a dielectric- lled groove. Fig. 6 illustrates the behaviors of a normalized backscattered echowidth versus an incident angle, i. It is seen that our higher-mode solutions (m = 2;4;6) agree well with 11]. A dominant-mode solution is accurate only near to the normal incidence (0 < i < 5 ). Fig. 7 shows the behaviors of a normalized radiationpattern versus an observation angle, for fteen rectangular grooves. Note that the geometry of fteen rectangular grooves is taken from 8]. Numerical computations are performed with seven modes (m = 6). The increase in the incident angle, i causes the increase in the mainbeam angle of fteen October 24, 2005 DRAFT
  • 8. 8 0 10 20 30 40 50 60 70 80 90 −15 −10 −5 0 5 10 15 Incident angle, θ i [Degree] Backscatteredechowidth,σ/λ 0 [dB] m = 0 m = 2 m = 4 m = 6 [11] Fig. 6. Behaviors of a normalized backscattered echowidth, = 0 versus an incident angle, i for a = 0:5 m], d = 0:25 m], f = 300 MHz], and 1 = 2 = 0. −90 −60 −30 0 30 60 90 −25 −20 −15 −10 −5 0 Observation angle, θ [Degree] Normalizedradiationpattern[dB] θi = 0o θi = 10o θi = 20o θi = 30o Fig. 7. Behaviors of a normalized radiation pattern versus an observation angle, for k1d = 1:57079628, a = 0:1d, N = 15, T(n) = 0:9d n=4;7;10;13 , T(n) = 0:4d n6=4;7;10;13 , and 1 = 2 = 0. October 24, 2005 DRAFT
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