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AFCRL-63-139 AD-A285 480 uN IN I N IM III I IIf! NI LEAKY WAVE RADIATION FROM A PERIODICALL SLOTTED WAVEGUIDE by Jean-Paul Renault Research Report PIBMRI- 1151-63 for Air Force Cambridge Research Laboratories Office of Aerospace Research United States Air Force Bedford, Mass. Contract No. AF-19(604)-7499 Project 4600, Task460004 May 8, 1963 L -. ° 94-24355 . / I N lHlllllltflllllllillIE WH~lill > '" EMRI1 POLYTECHNIC INSTITUTE OF BROOKLYN IJ1CROWAVE RESEARCH INSTITUTE ELECTROPHYSICS DEPARTMENT

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AFCRL-63-139

AD-A285 480uN IN I N IM III I I If! NI

LEAKY WAVE RADIATION FROM A PERIODICALL

SLOTTED WAVEGUIDE

by

Jean-Paul Renault

Research Report PIBMRI- 1151-63for

Air Force Cambridge Research LaboratoriesOffice of Aerospace Research

United States Air ForceBedford, Mass.

Contract No. AF-19(604)-7499Project 4600, Task460004

May 8, 1963

L

-. °

94-24355 . /I N lHlllllltflllllllillIE WH~lill > •'" EMRI1

POLYTECHNIC INSTITUTE OF BROOKLYN

IJ1CROWAVE RESEARCH INSTITUTEELECTROPHYSICS DEPARTMENT

(

"Requests for additional copies by Agencies of the Departmentof Defense, their contractors, and other Government Agenciesshould be directed to the:

DEFENSE DOCUMENTATION CENTER (DDC)Cameron StationAlexandria, Virginia

Department of Defense contractors must be established for DDCservices or have their 'need-to-know' certified by the cognizantmilitary agency of their project or contract.

"All other persons and organizations should apply to the:

U.S. DEPARTMENT OF COMMERCEOFFICE OF TECHNICAL SERVICESWASHINGTON 25, D.C."

I 0 II

"AFCRL-63-139 Research Report No. PIBMRI-1151-63

LEAKY WAVE RADIATION FROM A PERIODICALLY

SLOTTED WAVEGUIDE

by

Jean-Paul Renault

Polytechnic Institute of BrooklynMicrowave Research Institute

55 Johnson StreetBrooklyn 1, New York

Research Report PIBMRI-1151-63Contract No. AF- 19(604)-7499

Project 4600Task 460004

May 8, 1963

Title PageAcknowledgmentAbstractTable of Contents16 pages of textDistribution

Jeffn-Paul Renaulte search Fellow

Approved by:KJAATr. =.arlin

Head, Electrophysks Dept.

forAir Force Cambridge Research Laboratories

Office of Aerospace ResearchUnited States Air Force

Bedford, Mass.

ACKNOWLEDGMENT

The author is pleased to acknowledge the generous assistance of his late

advisor, Prof. L. 0. Goldstone, who first suggested many of the ideas used in this

report.

The work reported herein was sponsored by the Air Force Cambridge Research

Laboratories, Office of Aerospace Research, United States Air Force, Bedford,

Massachusetts, under Contract No. AF-19(604)-7499.

ABSTRACT

A rectangular waveguide with transverse slots located periodically in the broad

wall is analysed by the transverse resonance procedure. The slots are replaced by

equivalent conductances and susceptances; these are used in the resonance equation

to obtain leaky and surface wave solutions.

The theoretical solutions for the complex axial propagation constant are found,

and these results are verified experimentally. The transverse resonance method of

solution is shown to present advantages over previously derived results.

TABLE OF CONTENTS

I. INTRODUCTION

(a) Methods of analysis of leaky wave structures

(b) Description of the problem

UI. ANALYSIS OF THE STRUCTURE

(a) Network representation

(b) Transverse resonance

1. Leaky wave solution

2. Surface wave solution

III. RESULTS

(a) Theoretical

(b) Experimental

1. Amplitude measurements

2. Phase measurements

IV. CONCLUSION

I. INTRODUCTION

Leaky waves in many cases of practical interest are excited in lossless wave-

guides in which are cut either uniform or periodic apertures. These waves, whichhave a complex propagation constant, propagate along the leaky structure with aveloc-

ity greater than that of light and are continuously attenuated, indicating the leakage

of energy they undergo as they travel. The theoretical discussion of leaky wave struc-

tures using only field considerations would, therefore, generally be extremely arduous,

including particularly the solution of a discontinuity problem. But leaky waves are

solutions of the source-free field equations, so their propagation constants can be cal-

culated rigorously by means of a transverse resonance procedure. This procedure

includes two steps: first it is necessary to find a transverse network representation,

and then a resonance equation has to be solved. The first step consists mostly of

evaluating the discontinuities. Generally, however, this does not need to be carried

out since the results are already available in the literature. The next step consists of

the solution of a network problem. The resonance equation is a complex transcendental

equation which requires the use either of a computing machine or of numerical methods.

However, when the solution can be regarded as a perturbation of the propagation con-

stant of the closed waveguide, a perturbation technique may be uscýd which leads to

solutions in closed form where the functional behavior is immediately evident.

The theory of this network approach has already been discussed (1) and theevaluation of discontinuities has been carried out in many cases of practical interest(2)

In this report a transverse resonance procedure will be applied to a transversely-

slotted rectangular waveguide as illustrated in Figure 1.

a

Figure 1. Transversely- slotted waveguide

(1) L. 0. Goldstone and A. A. Oliner, " Leaky-wave Antennas I: Rectangular Wave-guides, " Research Report R-606-57, PIB 534 M. R.I.; August 57

(2) N. Marcuvitz, " Waveguide Handbook", Rad. Lab. Series, Vol. 10, McGraw-HillBook Co., New York, 1951

The structure consists of an array of closely-spaced transverse slots which extendcompletely across the broad face of a rectangular waveguide. The waveguide isassumed to be infinite, and its slotted face is inserted in an infinite conducting p1.-ne.

(3)This struc';ure is well 1.-iown and has already been studied by R. F. HynemanHowever, it will be discussed here from a completely different point of view. Where-as Hyneman started from the general field equations and used iterative techniqueswith computing machines to get numerical results, in the following analysis a simple

perturbation technique will be used to obtain simple closed form expressions for theguide wavelength and attenuation constant.

Experimental measurements have also been made of the attenuation constant andguide wavelength, and these measured results are compared with the theoretical ex-pressions. It is found that very good agreement is obtained with the presently-derivedtheory, but that the calculations of Hyneman differ considerably from the measuredvalues. Furthermore, Hynernan indicates that a surface wave is prcsent on this struc-ture, but the present theory finds no evidence of the presence of such a wave. These

points are considered in detail below.

(3) R. F. Hyneman, " Closely-Spaced Transverse Slots in Rectangular Waveguide"IRE Transactions on Antennas and Propagation, Nb 4, pp. 335-342, October 1959.

3

I. ANALYSIS OF THE STRUCTURE

A few restrictions have to be made in order to simplify the analysis of the

problem. First, if the propagation constant of the leaky wave is to be regarded as a

perturbation on the closed waveguide propagation constants, the slots have to be small,

i. e., the ratio of length to width a/ d must be sufficiently great, the ratio of width to

free space wavelength d/k sufficiently small, and the spacing of the slots must be

large compared to their width. Under these conditions the only appreciable component

of the tangential electric field in the apertures is the z component and the characteris-

tics of the wave traveling on the structure are only slightly different from those of the

unperturbed case and are thus susceptible to analysis by perturbation methods.

Then, if this structure is to exhibit a leaky-wave behavior, the leakage of energy

has to be uniform. In other words, the structure has to be regarded as radiating

continuously and not as a discrete array of apertures. This will be the case if the

slots spacing is very small with respect to the free-space wavelength (I < Xi.

(a) Network Representation

A slotted guide where only one leaky wave propagates can, when viewed trans-

versely, be represented by a single length of transmission line short-circuited at one

end and terminated at the other end in an appropriate lumped network representing the

discontinuity.

It has already been mentioned that the only appreciable component of the tangen-

tial electric field is the z component, so that the mode propagating in the slotted

waveguide can be regarded as a perturbation on a TE mode propagating in the y

direction (H type mode (i) ); besides, "a" and "b" can be chosen such that only the

fundamental H type modes are never coupled on such structures 1), so that at the dis-

continuity the only modes which are excited are H-type modes of all orders, the low-

est one being the only one to propagate. Therefore, the waveguide viewed transversely

can be represented by a single piece of transmission line of length b, short circuited

at one end and terminated in the appropriate lumped network which will be determined

later. In fact, this single transmission line picture is valid only if b is large enough

so that none of the decaying modes can reach the back wall and be reflected with an

appreciable amplitude.

E = E 0 sin ( Ya exp (-jkzz) (1.1)

The z dependence is the usual exp (-jkzz) dependence and the y dependence is

assumed to be very similar to sin gy/a, the y dependence in the closed waveguide.

4

Ez between the slots, at x= b is equal to zero. Due to the periodicity of this

structure an expansion of Ez in a Fourier series can be carried out which yields the

following expression

+W0

E= Y a sin 1-a exp -jkz7 exp -j (pnf z/ ) (1.1z L n a Zn-- -so

If K is the transverse wave number, corresponding to each n there will be a Kn

such as

K k 2 g/a)2 - (kz + "-( )2 (1.3)n - (na -( 2ij

where kis replaced by k + 2nri , according to Eq. (1.2). Dut k does not differwhr z is repace by kz --

very much from k zO for which2

k2 - i_ + e , (1.4)a? z 0

and I is much smaller than X, k = 2m/X is much smaller than :r /I ). Therefore,

except for n 0, which corresponds to the lowest leaky mode, Kn is approximately

equivalent to -j(2,T n/1) and the corresponding modes decay rapidly away from the

plane x = b. Even for n= I this will be true since I and b are of the same order

at x = -b and the fields are too highly attenuated to be appreciably reflected, thus

justifying the single transmission line picture. The preceding discussion shows that

the electromagnetic energy is partly stored in the neighborhood of the discontinuities,

which corresponds to the decaying modes, and partly radiated away.

In the lumped network the radiated energy is represented by a conductance G

and the stored energy by a suspectance jB as illustrated in Fig. 2.

Fig. 2: Transverse equivalent network.

1. Determination of G

The conductance G could be found by computing the power radiated far from the

antenna. But the lowest H-type mode (n 0 in (1.3) ), being the only one which is

propagating, is the only mode which contributes to the power radiated in the far zone.

Therefore, in the determination of G we can disregard all the space harmonics, and,

in so far as G is concerned, the tangential electric field in the aperture can be taken

as

Ez = 0 sinLaY exp -jk z (1. )

Z a

Fig. 3: Parallel plate waveguideradiating into half-space

This corresponds to the situation represented in Fig. 3: G is the admittance equi-

valent to a parallel plate waveguide radiating into half space with the electric field

parallel to the guide walls. The conductance G is given by (4)

G P 0.8' - (1.6)

where Y0 is the characteristic admittance of the parallel plate waveguide and the

K the transverse wavenumber given by

-22 (1.7)

(1.6) can be rewritten

G G 2

- 1.6 where Go= 0. p85 _-57 (1.8)K

and G does not depend on K.

(4) N. Marcuvitz, ' Waveguide Handbook", Rad. Lab. Series, Vol. 10, McGraw-HillBook Co., New York, 1951, p. 191 Eq. 2b.

6

2. Determination of B

The attenuated modes, although not contributing to the power radiated, contrib-ute to the stored energy which is represented in the network by the susceptance jB.The fields corresponding to these modes have appreciable values only in a fairlylimited region which does not extend far from the slots. It is therefore possible toconsider that the field distribution depends mostly on the geometry of the slots andvery little on the surrounding region. Accordingly, it does not make much differenceif we replace the structure represented in Fig. 4. a, (which is the actual structurestudied here) by the structure of Fig. 4. b.

(a)b)

Figure 4: Equivalent Radiating Structures

Clearly this is not completely rigorous since the field distributions corresponding tothe decaying modes in the structures illustrated above are likely to differ slightly.However, the results derived from this approximation yield results in excellent agree-

ment with experimental data.Furthermore the parallel plate waveguide with an array of transverse slots cut

in a plane perpendicular to its walls as illustrated in Fig. 4. b has for an image anarray of infinite slots cut in an infinite conducting plane. The suscepcance of such adiscontinuity with tangential magnetic field parallel to the edges of the slots is found

to be(5)

"B 2M1 I n cac ,-d (1.9)

0

which can be rewritten

B = BOK (l.9a)0

(5) N. Marcuvitz, "Waveguide Handbook", Rad. Lab. Series, Vol. 10, McGraw-HillBook Co., New York, 1951, p. 280 Eq. la.

7

where Bo - __ .n csc (r d/2t), (which does not depend on K).

(b) Transverse resonance

The second part in this problem is to determine K from the network representa-tiorn by meanp of a resonance procedure. The resonance equation can be written :n the

following manner

Y(K) = Y(K) + Y(K)= 0 (2.10)where Y (K) is (see Fig. 2) the admittance of the short-circuited piece of transmissionline i. e. -j Y0 cot K b and Y(K) the net admittance of the lumped network represen-ting the discontinuities i. e. G + jB. Therefore (2.10) becomes

-j Y0 cot Kb + jB + G =0 (2.11)

or

GO-j cot K b + jB 0 K + IF = 0 (2.12)

thus,Go

cot Kb= B 0K -j K (2.13)

and dividing both sides by Kb, we see that

cot Kb B0 G0 (2.14)K B = T- K2-b

Let xb = u, Eq. 2.14 becomes

cot ub B0 G0 b (215)U -Ju

This resonance equation should identical to the equation obtained by Hyneman(b) inwhich he started from %.he field equations. But whereas the left-hand sides are iden-tical, the right-hand side is here in a simple compact form as opposed to Hyneman'swhich uses a product of complicated series and integrals. However, once theseintegrals and series are evaluated the results should be the same, since in the Wave-guide Handbook the discontinuities were evaluated from the field equations. One ofthe principal advantages of the approach used here is that it does not carry out these

complicated computations and uses results already available.

(6) See Ref. no. (3) Eq. 14 p. 337.

8

1. Leaky-wave solutions

It is clear from Eq. 2.14 that the solution for K has to be complex, corres-

ponding to a leaky-wave solution. Since the slots are small (Sec. Ia) the solution K

of 2.14 can be regarded as a perturbation on the dominant H10 mode in a completely

closed waveguide for which there is no x dependence, and therefore K = 0. Thus, it

is expected that the resonant value of K and accordingly of u will be small. So, in

order to find the value of K for the lowest leaky-wave on the structure, the left hand

side of Equation (2.15) can be expanded in powers of u = Kb, keeping only the first

two terms and neglecting terms of higher order.

1 u2 1I u2 u2 1 ucoo u 2 u u I -+ )cot U = I%----u = +

uU-

so (7)

cotu 1 1(u 2 (.6u

Substituting in (2.15), we get

1 1 B 0 G 0 bu2 - -u- 2 -j

or

u2 -=B0 u2 -j G0 b (2.18)3 b

Using K= u/b

2 1 +j G 0 b (2.20)b2 B 0 +

b 3

So K can be calculated, taking the square root of K2 with positive real and imaginary

part which indicates the leaky-wave behavior. From K, kz can be found as

kz = j - = k 2 - ('l)2 - K 2 (2.21)

z a

where a is the attenuation constant per unit length and 1 the phase shift per unit

(7) The first term neglected in the expansion of (cot u/u) is (-u 2 /45). Since in

most cases of interest Jul turns out to be close to 1 this approximation is

generally better than 5% accurate.

nmmummmm m||~ m m II II l INIw

9

length (in thc z-direction). Dividing both sides of (2. 21) by k = 2A / yields

X a - /2a - (KX/2t (2.??)

g

Xg is the guide wavelength Xg = 2 . Therefore

K- Re - ( (2.23)

gand

ak = -24 )m 1- (k/2a)2 1 (K/2 )2 (4)

In cases considered here where IKI is small, a more explicit functional

dependence can be obtained by means of a perturbation method. Let kzO be the

longitudinal wavenumber for the closed waveguide

kz0 k 2 -(t/a) 2 , (2-25)

and (2.21) can be rewritten

k =t-jCz= k 2 _ K2 (2.26)z zO

kz - k i 2 (2.27)zO

(K/kz0)2

which can be expanded in a power series of K2 /kz 02 which is, neglecting t -ns of

higher order than / k 2

kz ,Z K2 2 (2.28)

2kz

Hence

- K2 (2.28a)kz kz0 V

Substituting for K2 the value given by Eq. (2.20)

k 1 1+ jGb (2.29)z zo 2 b2k BBO +(S b 3

from which a is evaluated as

10

a= 0___ (2.30)

bkzo Bo +b 3

then

-X- B 0- (2.31)2bkz0 0 1

b 3

or

X= 0 B 0 (2.31 a)0_ +!B

b 3

where X go is the closed guide wavelength. Similarly for Ps

k ~ B (2.32)kz0 2b 2 k3 0 1 BO

3 b

or

XXX X .. go 1 (2.32a)

2 Bog gO 8, 2 b2 1 + 0

3 b

2. Surface wave solution

It is clear that Equation (2.14)

cot K b B 0 0 (214colb - (2.14)

K2b

does not admit any real or purely imaginary solution for K. Therefore, in so far as

the network representation derived in Sec. Hia is valid, there cannot be at the same

time a leaky-wave and a surface wave supported by the structure considered here.(8)

This is in contradiction with what Hyneman seemed to have observed.

Moreover if a surface wave was to be excited alone there would be no power

radiated at infinity and the term in G of Eq. a14 would vanish. Eq. (2.14) would

reduce to

cot Kb B0 (2.33)

(8) See Reference no. (3) Sec. D., pp. 339, 340.

11

0.40 -.70 -

0.30

0.20 PARAMETER

0.08

0.06

0.04

0.02

""--0.95

0.01 NETWORK PROCEDURE - - -

0.445 *"So 12 -7-r

0033

HYNEMAN

b = 0.466

d = 0.033

0.1 0.2 0.3 0.4

Fig.5. THEORETICAL ATTENUATION vs.SLOT SPACING IN WAVELENGTHS M.R.1.- 19103

12

2/

ANTENNA PARAMETERSa 0.9"*"", -_ b -0.4" 11o..-- 1 I.0.30 ~

0.8 d 0.032" -

(nepers) /

-THEORETICAL RESULTSX EXPERIMENTAL RESULTS

-- HYNEMAN'S RESULTS

0.7 0.8 0.9

2a

Fig.6. ATTENUATION vs. WAVELENGTH

1.0

-- THEORETICALERETCL

0xEXPERIMENTAL

0.6---------------

OA

ANTENNA PARAMETERS __

a = 0.9"10.2- b =0.4' _ _

L = 0.3"i

0.01 ,d = 0.032"0.40.60 .0.6 0.7S 0.8

2a

Fig.7. vs. WAVELENGTHg

M.R.I.-19104

13

II. RESULTS

a. Theoretical Results

Froni the expression (2.24) the normalized attenuation constant a/k = 0•k/Pt

was computed. The results are plotted on Fig. 5 for several values of a /X, ver-

sus the spacing of the slots 1/X. On the same figure are compared the results

obtained by Hyneman for a waveguide only slightly different: the obviously disagree.

On Fig. 6 the plots of attenuation constants Ca versus X/2a are found first

as computed from Eq. (2.24) and then from the perturbational expression as in (2. 31)

(2.31). The discrepancy between these two curves, though increasing with the wave-

length, is always relatively small. In fact, whereas neglecting u2 /45 in the

expansion of cot u/u is an excellent approximation since lul is found to be close

to 1, it is not such a good approximation to neglect terms of the order K4 (8k 0 ) in

the expansion of kz in (2.27) because for b= 0.4", IKI = Iul/b is equivalent to

IKd Z 2.5.In any case, the perturbation expression is a far better approximation than

Hyneman' s results( 8 ) which are plotted on the same figure and show clearly the

functional dependence of the leaky-wave characteristics.

Finally on Figure 7 X/(Xg) versus X/2a is plotted as given by Eq. (2.23).

b. Experimental Results

An antenna of the type described in the introduction of this report was construc-

ted as illustrated in Fig. 8.

0.4"

S~~~20 -

Fig. 8 Antenna constructed for the measurements.

(8) There were only two points available in Hynenian' s report (Ref. (3)) to plot the

curve of Fig. 6.

14

In order to avoid reflections at the open end of the guide, the length of the

antenna was taken to be around 20 wavelengths so that no wave reach the end with

an appreciable amplitude. In addition, it was found necessary to increase progres-

sively the length of the slots, because if they all extended completely across the broad

face, the discontinuity in the neighborhood of the first ones could be important enough

to excite a strong space-wave which would almost conceal completely the leaky wave.

The waveguide was inserted in a large aluminum ground plane 8' X 8' and

radiated into a microwave darkroom approximately 10' X 10' X 10' the walls of

which were covered with an absorbing material. The probe consists of a length of

flexible miniature coaxial cable which is supported by a polyfoam structure and is

covered by absorbing material to minimize as much as possible the distortion of the

field. The probe carriage is motor driven and its travel is controlled by limit swit-

ches and a reversing switch.

I. Attenuation measurements.

The probe is oriented perpendicularly to the slotted face of the antenna. The

signal available from the probe is fed to a recorder through a DC amplifier (Fig. 9).

As the probe travels along the antenna at a uniform speed, the recorder plots the

amplitude distribution of the leaky wave. These data are plotted on semi-log graph

paper, the slope of the straight line which best fits a particular set of data is used to

compute the attenuation constant. The results so obtained are shown on Fig. 6.

2. Phase measurements.

The phase measurements are taken with the configuration slightly modified. A

null method is used to compare the phases of the aperture field and of a reference

signal. The magnitude and phase of this reference are adjusted by means of a cali-

brated attenuator and a slotted section. Comparison of the phases is accomplished by

a hybrid tee junction. A block diagram of the set up used here is shown in Fig. 10.

The experimental values of the guide wavelength are plotted on Fig. 7.

GROUND PLANE

LEAKYGUIDE

SLIDEPRBAN

DIRECTIONAL SCREW PROBE ANDISOLATOR COUPLER TUNER iDETECTOR

KLYSTRON 'J'ý r

WAVEMETER

RECORDER AMPLIFIER

Fig. 9 Block diagram of equipment for attenuation measurement.

GROUND PLANE

LEAKYGUIDE TRAVERSE

SLIDE

DIRECTIONAL SCREW IPROBEISOLATOR COUPLERS TUNER | (NO CRYSTAL)

KLYSTRON

WAVE METER

CALIBRATED MATCHEDAT TENUATOR LOAD

SLOTTEDSECTION

HYBRID T

MATCHED CRYSTAL ANDLOAD AMPLIFIER

Fig. 10 Block diagram of equipment for guide wavelength measurement.

MRI- 19105

16

IV. CONCLUSIONS

The experimental results obtained for the attenuation constant and the guide

wavelength agree very satisfactorily with the theoretical values (see Fig. 6 and 7).

This fact shows that those approximations which were made in Section ia were

perfectly justified.

The validity of the network representation used here seems therefore to be fully

guaranteed, and the results derived therefrom are in far better agreement with

measured values than any results previously derived by other methods.

Furthermore, it becomes very doubtful that this structure could excite a surface

wave together with a leaky wave, as indicated by Hyneman.

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Scientific and Technical Info. Facility Hq. AFCRL, OARAttn: NASA Representative (S-AK/ DL) (CRXR, J. R. Marple)Post Office Box 4700 L.G. Hanscom Field,Bethseda, Md. 1 Bedford, Mass.

National Bureau of Standards Chief,U.S. Department of Commerce Bureau of ShipsWashington 25, D.C. Department of the NavyAttn: G. Shapiro (Chief, Eng. Elec. Washington 25, D.C.Sec. Electricity and Electronics Attn: Code 690Division) 1

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Director Aero Geo Astro Corp.U.S. Naval Research Labs. 1200 Duke StreetWashington 25, D.C. Alexandria, Va.Attn: Code 2027 2 Attn: Library

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Chu AssociatesBell Telephone Labs. P.O. Box 387Murray Hill, N.J. Whitcomb Avenue

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