lecture 26 te and tm waves

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EECS 117  Lecture 26: TE and TM Waves Prof. Niknejad University of California, Berkeley University of California, Berkeley EECS 117 Lecture 26 p. 1/  

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Page 1: Lecture 26 TE and TM Waves

8/2/2019 Lecture 26 TE and TM Waves

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EECS 117

 Lecture 26: TE and TM Waves

Prof. Niknejad

University of California, Berkeley

University of California, Berkeley EECS 117 Lecture 26 – p. 1/

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TE Waves

TE means that ez = 0 but hz = 0. If kc = 0, we can useour solutions directly

H x =− jβ 

k2c

∂hz∂x

H y =− jβ 

k2c

∂hz∂y

E x = − jωµk2c

∂hz∂y

E y = − jωµk2c

∂hz∂x

Since kc = 0, we find hz from the Helmholtz’s Eq.

∂ 2

∂x2+

∂ 2

∂y2+

∂ 2

∂z2+ k2

H z = 0

University of California, Berkeley EECS 117 Lecture 26 – p. 2/

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TE Wave Helmholtz Eq.

Since H z = hz(x, y)e− jβz

∂ 2

∂x2+ ∂ 

2

∂y2−β 2 + k2   

k2c

hz = 0

Solving the above equation is sufficient to find all thefields.

We can also define a wave impedance to simplify the

computation

Z TE  =E xH y

=−E yH x

=ωµ

β 

University of California, Berkeley EECS 117 Lecture 26 – p. 3/

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Wave Cutoff Frequency

Since β  = 

k2 − k2c , we see that the impedance is not

constant as a function of frequency.

In fact, for wave propagation we require β  to be real, ork > kcω√

µǫ > kc

ω > kc√µǫ

= ωc

For wave propagation, the frequency ω must be larger

than the cutoff frequency ωc

Thus the waveguide acts like a high-pass filter

University of California, Berkeley EECS 117 Lecture 26 – p. 4/

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TM Waves

Now the situation is the dual of the TE case, ez = 0 buthz = 0

Our equations simplify down to

H x =jωǫ

k2c

∂ez∂y

H y =− jωǫ

k2c

∂ez∂x

E x =− jβ 

k2c

∂ez∂x

E y =− jβ 

k2c

∂ez∂y

And for kc = 0, our reduced Helmholtz’s Eq. for E z

∂ 2

∂x2

+∂ 2

∂y2

+ k2c ez = 0

University of California, Berkeley EECS 117 Lecture 26 – p. 5/

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TM Wave Impedance

With ez known, all the fields can be derived from theabove equations

The wave impedance is given by

Z TM  =E xH y

=−E yH x

=β 

ωǫ

Since β  = 

k2 − k2c , we see that the impedance is not

constant as a function of frequency.

The same high-pass cutoff behavior is also seen withthe TM wave

University of California, Berkeley EECS 117 Lecture 26 – p. 6/

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TE/TM Wave General Solution

1. Solve the reduced Helmholtz eq. for ez or hz

2. Compute the transverse fields

3. Apply the boundary conditions to find kc and anyunknown constants

4. Compute β  =

 k2 − k2

c , so that γ  = jβ  and Z TM  = β ωǫ

University of California, Berkeley EECS 117 Lecture 26 – p. 7/

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Parallel Plate Waveguide

x

y

z

dµǫ

w

Consider a simple parallel plate waveguide structure

Let’s begin by finding the properties of a TEM mode ofpropagation

Last lecture we found that the TEM wave has an

electrostatic solution in the transverse plane. We canthus solve this problem by solving Laplace’s eq. in theregion 0 ≤ y ≤ d and 0 ≤ x ≤ wn

∇2Φ = 0

University of California, Berkeley EECS 117 Lecture 26 – p. 8/

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Voltage Potential of TEM Mode

The waveguide structure imposes the boundaryconditions on the surface of the conductors

Φ(x, 0) = 0

Φ(x, d) = V 0

Neglecting fringing fields for simplicity, we haveΦ(x, y) = Ay + B

The first boundary condition requires that B ≡ 0 and thesecond one can be used to solve for A = V 0/d.

University of California, Berkeley EECS 117 Lecture 26 – p. 9/

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Transverse Fields of TEM Mode

E

H

ρs =Dn

J s = H t

The electric field is now computed from the potential

e(x, y) = −∇tΦ = −∂ Φ

∂xx + ∂ Φ

∂yy

= −yV 0d

E = e(x, y)e− jβz = −yV 0d

e− jkz

H =z× E

Z TEM 

= xV 0

e− jkz

University of California, Berkeley EECS 117 Lecture 26 – p. 10/

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Guide Voltages and Currents

The E  and H  fields are shown above. Notice that thefields diverge on charge

ρn = n ·D = ǫ V 0d

e− jkz

This charge is traveling at the speed of light and giving

rise to a current

I  = ρnwc = w1√ǫµ

ǫV 0ηd

e− jkz =wV 0ηd

e− jkz

University of California, Berkeley EECS 117 Lecture 26 – p. 11/

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Guide Currents

We should also be able to find the guide current fromAmpère’s law

I  =  C b

H · dℓ = wH x = wV 0ηd

e− jkz

This matches our previous calculation. A third way to

calculate the current is to observe that J s = H t

I  =  w

0

Js · zdx =wV 0ηd

e− jkz

The line characteristic impedance is the ratio of voltageto current

Z 0 = V I  = V 0 ηdwV 0= η dw

University of California, Berkeley EECS 117 Lecture 26 – p. 12/

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Guide Impedance and Phase Velocity

The guide impedance is thus only a function of thegeometry of the guide. Likewise, the phase velocity

v p = ωβ 

= ωk

= 1√µǫ

The phase velocity is constant and independent of the

geometry.

University of California, Berkeley EECS 117 Lecture 26 – p. 13/

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TM Mode of Parallel Plate Guide

For TM modes, recall that hz = 0 but ez = 0

We begin by solving the reduced Helmholtz Eq. for ez

∂ 2

∂x2+ ∂ 2

∂y2+ k2

c

ez(x, y) = 0

where k2

c = k2

− β 2

. As before, we take∂ 

∂x = 0 forsimplicity

∂ 2

∂y2

+ k2c ez(x, y) = 0

The general solution of this simple equation is

ez(x, y) = A sin kcy + B cos kcy

University of California, Berkeley EECS 117 Lecture 26 – p. 14/

TM M d B d C di i

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TM Mode Boundary Conditions

Even though ez = 0 inside the guide, at the boundary ofthe conductors, the tangential field, and hence ez mustbe zero.

This implies that B = 0 in the general solution. Also,applying the boundary condition at y = d

ez(x, y = d) = 0 = A sin kcdThis is only true in general if kc = 0. But we havealready seen that this corresponds to a TEM wave. We

are now interested in TM waves so the argument of thesine term must be a multiple of nπ for n = 1, 2, 3, . . .

kcd = nπ→

kc =nπ

d

University of California, Berkeley EECS 117 Lecture 26 – p. 15/

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Axial Fields in Guide

The propagation constant is thus related to thegeometry of the guide (unlike the TEM case)

β  = 

k2 − k2c =

 k2 − nπ

d2

The axial fields are thus completely specified

ez(x, y) = An sinnπy

d

E z(x,y,z) = An sinnπyd

e− jβz

University of California, Berkeley EECS 117 Lecture 26 – p. 16/

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Transverse TM Fields

All the other fields are a function of E z

H x =− jωǫ

k2c

∂E z

∂y

H y =− jωǫ

k2c

∂E z∂x

E x =− jβ 

k2c

∂E z

∂x

E y =− jβ 

k2c

∂E z∂y

So that H y = E x = 0 by inspection. The othercomponents are

H x = jωǫkc

An cosnπy

d

e− jβz

E y = − jβ 

kc An cosnπy

d e

− jβz

University of California, Berkeley EECS 117 Lecture 26 – p. 17/

C t ff F

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Cutoff Frequency

As we have already noted, for wave propagation β  must

be real. Since β  = 

k2 − k2c , we require

k > kc

ω√ǫµ > kc

ω > kc√µǫ

= ωc

ωc =nπ

d√µǫ

The guide acts like a high-pass filter for TM modeswhere the lowest propagation frequency for a particularmode n is given by

f c =n

2d√µǫ

=nc

2d

=n

λg

University of California, Berkeley EECS 117 Lecture 26 – p. 18/

TM M d V l it d I d

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TM Mode Velocity and Impedance

The TM mode wave impedance is given by

Z TM  =−E y

H x=

β 

ωǫ

=β √

µǫ

ωǫ√µǫ

= β √

µǫkǫ =βη

k

This is a purely real number for propagation modesf > f c and a purely imaginary impedance for cutoff

modes

The phase velocity is given by

v p = ωβ  = ωk

 1−

kck

2 = c 1−

kck

2 > c

The phase velocity is faster than the speed of light!Does that bother you?University of California, Berkeley EECS 117 Lecture 26 – p. 19/

Ph V l it

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Phase Velocity

It’s important to remember that the phase velocity is arelationship between the spatial and time componentsof a wave in steady-state . It does not represent the

wave evolution!Thus it’s quite possible for the phase to advance fasterthan the time lag of “light” as long as this phase lag is a

result of a steady-state process (you must wait aninfinite amount of time!)

The rate at which the wave evolves is given by the

group velocity

vg =

dβ 

−1

≤ c

University of California, Berkeley EECS 117 Lecture 26 – p. 20/

P Fl

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Power Flow

Let’s compute the average power flow along the guidefor a TM mode. This is equal to the real part of thecomplex Poynting vector integrated over the guide

P 0 =1

2ℜ w0

 d0

E×H∗ · zdydx

z · E×H∗ = E yH ∗x =− jωǫ

kc

An cos

nπy

d

2 − jβ 

kc

=ωǫβ 

k2c

A2

n cos2

nπy

d

University of California, Berkeley EECS 117 Lecture 26 – p. 21/

Power Flow (cont)

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Power Flow (cont)

Integrating the cos2 term produces a factor of 1/2

P 0 =1

4

wωǫd

k2

c |An

|2

ℜ(β )

Therefore, as expected, if f > f c, the power flow isnon-zero but for cutoff modes, f < f c, the average

power flow is zero

University of California, Berkeley EECS 117 Lecture 26 – p. 22/