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to the resistance R; i.e., X ≈ R≈ l σ(δs2πa) (4.20) This is unique to good conductors at AC; that is, we see no such reactance at DC. Because this reactance is positive, it is often referred to as an inductance. However, this is misleading since inductance refers to the ability of a structure to store energy in a magne...
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δs ≪ a. The utility of this description is that it facilitates the modeling of wire reactance as an inductance in an equivalent circuit. Summarizing: A practical wire may be modeled using an equiv- alent circuit consisting of an ideal resistor (Equa- tion 4.17) in series with an ideal inductor (Equa- tion 4.22). Wherea...
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explained in Section 3.11. Example 4.2. Equi valent inductance of the inner conductor of RG-59. Elsewhere in the book we worked out that the inductance per unit length L′ of RG-59 coaxial cable was about 370 nH/m. W e calculated this from magnetostatic considerations, so the reactance associated with skin effect is not...
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54 CHAPTER 4. CURRENT FLOW IN IMPERFECT CONDUCTORS associated with skin effect is as important as the magnetostatic inductance in the kHz regime, and becomes gradually less important with increasing frequency . Recall that the phase velocity in a low-loss transmission line is approximately 1/ √ L′C′. This means that sk...
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for the impedance Zof a good conductor having width W, length l, and which is infinitely deep: Z ≈ 1 + j σδs · l W (A C case) (4.25) where σis conductivity (SI base units of S/m) and δs is skin depth. Note that δs and σare constitutive parameters of material, and do not depend on geometry; whereas land W describe geomet...
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Surface impedance ZS (Equation 4.26) is a ma- terials property having units of Ω/□, and which characterizes the AC impedance of a material in- dependently of the length and width of the mate- rial. Surface impedance is often used to specify sheet materials used in the manufacture of electronic and semiconductor devices...
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4.3. SURF ACE IMPEDANCE 55 Image Credits Fig. 4.1: c⃝ Sevenchw (C. W ang), https://commons.wikimedia.org/wiki/File:Current flow in cylinder new .svg, CC BY SA 4.0 (https://creativecommons.org/licenses/by-sa/4.0/). Fig. 4.2: Biezl, https://commons.wikimedia.org/wiki/File:Skin depth.svg, public domain. Modified from origin...
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Chapter 5 W a ve Reflection and T ransmission 5.1 Plane W aves at Normal Incidence on a Planar Boundary [m0161] When a plane wave encounters a discontinuity in media, reflection from the discontinuity and transmission into the second medium is possible. In this section, we consider the scenario illustrated in Figure 5.1:...
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intensity ˜Ei of this wave is given by ˜Ei(z) = ˆxEi 0e−jβ1z , z≤ 0 (5.1) where β1 = ω√ µ1ǫ1 is the phase propagation constant in Region 1 and Ei 0 is a complex-valued constant. ˜Ei serves as the “stimulus” in this problem. That is, all other contributions to the total field may be expressed in terms of ˜Ei. In fact, al...
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geometrical symmetry of the problem, which precludes waves traveling in any other directions. The symmetry of the problem also precludes a change of polarization, so the reflected wave should have no ˆy component. Therefore, we may be confident that the reflected electric field has the form ˜Er(z) = ˆxBe+jβ1z , z≤ 0 (5.3) ...
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5.1. PLANE W A VES A T NORMAL INCIDENCE ON A PLANAR BOUNDAR Y 57 where Bis a complex-valued constant that remains to be determined. Since the direction of propagation for the reflected wave is −ˆz, we have from the plane wave relationships that ˜Hr(z) = −ˆy B η1 e+jβ1z , z≤ 0 (5.4) Similarly , we infer the existence of ...
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respectively , in Region 2. The constant C, like B, is a complex-valued constant that remains to be determined. At this point, the only unknowns in this problem are the complex-valued constants Band C. Once these values are known, the problem is completely solved. These values can be determined by the application of bo...
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tangential component of the electric field across the boundary requires ˜E1(0) = ˜E2(0), and therefore ˜Ei(0) + ˜Er(0) = ˜Et(0) (5.9) Now employing Equations 5.1, 5.3, and 5.5, we obtain: Ei 0 + B = C (5.10) Clearly a second equation is required to determine both Band C. This equation can be obtained by enforcing the bo...
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steps are the same. W e define ˜H1 and ˜H2 to be the total magnetic field intensities in Regions 1 and 2, respectively . The total field in Region 1 is ˜H1(z) = ˜Hi(z) + ˜Hr(z) (5.11) The field in Region 2 is simply ˜H2(z) = ˜Ht(z) (5.12) The boundary condition requires ˜H1(0) = ˜H2(0), and therefore ˜Hi(0) + ˜Hr(0) = ˜Ht(...
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58 CHAPTER 5. W A VE REFLECTION AND TRANSMISSION incidence from Region 1 toward Region 2. W e may now solve for Cby substituting Equation 5.15 into Equation 5.10. W e find: C = (1 + Γ 12) Ei 0 (5.17) Now summarizing the solution: ˜Er(z) = ˆxΓ 12Ei 0e+jβ1z , z≤ 0 (5.18) ˜Et(z) = ˆx (1 + Γ 12) Ei 0e−jβ2z , z≥ 0 (5.19) Equ...
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A second case of practical interest is when Region 2 is a perfect conductor. First, note that this may seem at first glance to be a violation of the “lossless” assumption made at the beginning of this section. While it is true that we did not explicitly account for the possibility of a perfect conductor in Region 2, let...
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Thus, we obtained the correct answer because we were able to independently determine that η2 = 0 in a perfect conductor. When Region 2 is a perfect conductor, the reflec- tion coefficient Γ 12 = −1 and the solution de- scribed in Equations 5.18 and 5.19 applies. It may be helpful to note the very strong analogy between r...
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load, and the special case η2 = 0, also considered previously , is analogous to a short-circuit load. In the case of transmission lines, we were concerned about what fraction of the power was delivered into a load and what fraction of the power was reflected from a load. A similar question applies in the case of plane w...
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5.1. PLANE W A VES A T NORMAL INCIDENCE ON A PLANAR BOUNDAR Y 59 equal to the incident power density minus the reflected power density . Thus: St ave = Si ave − Sr ave = ( 1 − |Γ 12|2) Si ave (5.23) In other words, the ratio of power density transmitted into Region 2 to power density incident from Region 1 is St ave Sia...
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of permittivity for these media. Assuming µ= µ0, we find: Γ 12 = η2 − η1 η2 + η1 = √ µ0/ǫ2 − √ µ0/ǫ1√ µ0/ǫ2 + √ µ0/ǫ1 = √ǫ1 − √ǫ2 √ǫ1 + √ǫ2 (5.25) Moreo ver, recall that permittivity can be expressed in terms of relative permittivity; that is, ǫ= ǫrǫ0. Making the substitution above and eliminating all extraneous factors...
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Moon’s surface as a planar boundary between free space and a semi-infinite region of lossy dielectric material. The reflection coefficient is given approximately by Equation 5.26 with ǫr1 ≈ 1 and ǫr2 ∼ 3. Thus, Γ 12 ∼ − 0.27. Subsequently , the fraction of power reflected from the Moon relative to power incident is |Γ 12|2...
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60 CHAPTER 5. W A VE REFLECTION AND TRANSMISSION 5.2 Plane W aves at Normal Incidence on a Material Slab [m0162] In Section 5.1, we considered what happens when a uniform plane wave is normally incident on the planar boundary between two semi-infinite media. In this section, we consider the problem shown in Figure 5.2: ...
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For consistency of terminology , let us refer to the problem considered in Section 5.1 as the “single-boundary” problem and the present (slab) problem as the “double-boundary” problem. Whereas there are only two regions (“Region 1” and “Region 2”) in the single-boundary problem, in the double-boundary problem there is ...
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In both problems, we presume an incident wave in Region 1 incident on the boundary with Region 2 having electric field intensity ˜Ei(z) = ˆxEi 0e−jβ1z (Region 1) (5.28) where β1 = ω√ µ1ǫ1 is the phase propagation constant in Region 1. ˜Ei serves as the “stimulus” in this problem. That is, all other contributions to the ...
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be determined; and subsequently the reflected magnetic field intensity is: ˜Hr(z) = −ˆy B η1 e+jβ1z (Re gion 1) (5.31) Similarly , we infer the existence of a transmitted plane wave propagating in the +ˆz direction in Region 2. The electric and magnetic field intensities of this wave are given by: ˜Et2(z) = ˆxCe−jβ2z (Reg...
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5.2. PLANE W A VES A T NORMAL INCIDENCE ON A MA TERIAL SLAB 61 complex-valued constant that remains to be determined. Now let us consider the boundary between Regions 2 and 3. Note that ˜Et2 is incident on this boundary in precisely the same manner as ˜Ei is incident on the boundary between Regions 1 and 2. Therefore, ...
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propagation constant and wave impedance, respectively , in Region 3. The constant F, like D, is a complex-valued constant that remains to be determined. W e infer no wave traveling in the (− ˆz) in Region 3, just as we inferred no such wave in Region 2 of the single-boundary problem. For convenience, T able 5.1 shows a...
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by enforcing boundary conditions on the electric and magnetic fields at each of the two boundaries. As in the single-boundary case, the relevant boundary condition is that the total field should be continuous across each boundary . Applying this condition to the boundary at z= 0, we obtain: ˜Et2(0) + ˜Er2(0) = ˜Et(0) (5....
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Equations 5.42–5.45 are recognizable as a system of 4 simultaneous linear equations with the number of unknowns equal to the number of equations. W e could simply leave it at that, however, some very useful insights are gained by solving this system of equations in a particular manner. First, note the resemblance betwe...
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62 CHAPTER 5. W A VE REFLECTION AND TRANSMISSION Electric Field Intensity Magnetic Field Intensity Region of V alidity Region 1 ˜Ei(z) = ˆxEi 0e−j β1z ˜Hi(z) = + ˆy ( Ei 0/η1 ) e−jβ1z z≤ − d ˜Er(z) = ˆxBe+jβ1z ˜Hr(z) = −ˆy (B/η1) e+jβ1z Region 2 ˜Et2(z) = ˆxC e−jβ2z ˜Ht2(z) = + ˆy (C/η2) e−jβ2z −d≤ z≤ 0 ˜Er2(z) = ˆxDe+...
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two unknowns – a dramatic simplification! However, even this is more work than is necessary , and a little cleverness at this point pays big dividends later. The key idea is that we usually have no interest in the fields internal to the slab; in most problems, we are interested merely in reflection into Region 1 from the ...
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in Regions 2 or 3 of the original problem, so we define a new wave impedance ηeq to represent this new condition. If we can find an expression for ηeq, then we can develop a solution to the original (two-boundary) problem that looks like a solution to the equivalent (simpler, single-boundary) problem. c⃝ C. W ang CC BY -...
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Bringing the factor of η2 to the front and substituting D= Γ 23C: ηeq = η2 Ce+jβ2d + Γ 23Ce−jβ2d Ce+jβ2d − Γ 23C e−jβ2d (5.54) Finally , we divide out the common factor of Cand multiply numerator and denominator by e−jβ2d,
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5.2. PLANE W A VES A T NORMAL INCIDENCE ON A MA TERIAL SLAB 63 yielding: ηeq = η2 1 + Γ 23e−j2β2d 1 − Γ 23e−j2 β2d (5.55) Equation 5.55 is the wave impedance in the re- gion to the right of the boundary in the equiva- lent scenario shown in Figure 5.3. “Equivalent” in this case means that the incident and reflected field...
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the complex value of the wave impedance is not indicating loss. Instead, the non-zero phase of ηeq represents the ability of the standing wave inside the slab to impart a phase shift between the electric and magnetic fields. This is precisely the same effect that one observes at the input of a transmission line: The inp...
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Figure 5.3: Γ 1,eq ≜ ηeq − η1 ηeq + η1 (5.56) The quantity Γ 1,eq may now be used precisely in the same way as Γ 12 was used in the single-boundary problem to find the reflected fields and reflected power density in Region 1. 2 See the section “Input Impedance of a T erminated Lossless Transmission Line” for a reminder. Th...
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3 as approximately free space, and Region 2 as the pane. Thus η1 = η3 = η0 ∼= 376.7 Ω (5.57) and η2 = η0 √ǫr ∼ = 188 .4 Ω (5.58) The reflection coefficient from Region 2 to Region 3 is Γ 23 = η3 − η2 η3 + η2 = η0 − η2 η0 + η2 ∼= 0.3333 (5.59) Gi ven f = 2.45 GHz, the phase propagation constant in the glass is β2 = 2π λ ...
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64 CHAPTER 5. W A VE REFLECTION AND TRANSMISSION The ratio of reflected power density to incident po wer density is simply the squared magnitude of this reflection coefficient, i.e.: Sr ave Siav e = |Γ 1,eq |2 = 0.292 ∼= 29.2% (5.63) where Sr av e and Si ave are the reflected and incident power densities, respectively . Si...
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from the z= −dinterface must be transmitted into Region 3. In other words: St ave Siav e = 1 − |Γ 1,eq |2 (5.65) where St av e is the transmitted power density . Example 5.3. Transmission of WiFi through a glass pane. Continuing Example 5.2: What fraction of incident power passes completely through the glass pane? Solu...
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loss, so that the media in each region is characterized entirely by permittivity and permeability . W e now focus on a particular class of applications involving this structure. In this class of applications, we seek total transmission through the slab. By “total transmission” we mean 100% of power incident on the slab...
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then shall provide some examples of these applications. W e begin with characterization of the media. Region 1 is characterized by its permittivity ǫ1 and permeability µ1, such that the wave impedance in Region 1 is η1 = √ µ1/ǫ1. Similarly , Region 2 is characterized by its permittivity ǫ2 and permeability µ2, such tha...
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5.3. TOT AL TRANSMISSION THROUGH A SLAB 65 the reflection coefficient Γ 1,eq = ηeq − η1 ηeq + η1 (5.67) where ηeq is given by ηeq = η2 1 + Γ 23e−j2β2d 1 − Γ 23e−j2 β2d (5.68) and where Γ 23 is given by Γ 23 = η3 − η2 η3 + η2 (5.69) T otal transmission requires that Γ 1,eq = 0. From Equation 5.67 we see that Γ 1,eq is zer...
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the numerator and denominator, we obtain: η1 = η2 (1 + P)η3 + (1 − P)η2 (1 − P)η3 + (1 + P)η2 (5.74) The parameters η1, η2, η3, β2, and ddefining any single-slab structure that exhibits total transmis- sion must satisfy Equation 5.74. Our challenge now is to identify combinations of parameters that satisfy this conditio...
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always 1, so the first value of P you might think to try is P = +1. In fact, this value satisfies Equation 5.75. Therefore, e−j2β2d = +1. This new condition is satisfied when 2β2d= 2πm, where m= 1,2,3,... (W e do not consider m≤ 0 to be valid solutions since these would represent zero or negative values of d.) Thus, we fin...
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the media in Regions 1 and 3 is that they have equal wave impedance. Example 5.4. Radome design by half-wave matching. The antenna for a 60 GHz radar is to be protected from weather by a radome panel positioned directly in front of the radar. The panel is to be constructed from a low-loss material having µr ≈ 1 and ǫr ...
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66 CHAPTER 5. W A VE REFLECTION AND TRANSMISSION used? Solution . This is a good application for half-wave matching because the material on either side of the slab is the same (presumably free space) whereas the material used for the slab is unspecified. The phase velocity in the slab is vp = c √ǫr ∼= 1.5 × 108 m/s (5.7...
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or decreases from the design frequency , there will be increasing reflection and decreasing transmission. Quarter-wave matching requires that the wave impedances in each region are different and related in a particular way . The quarter-wave solution is obtained by requiring P = −1, so that η1 = η2 (1 + P)η3 + (1 − P)η2...
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ing. Example 5.5. Radome design by quarter-wave matching. The antenna for a 60 GHz radar is to be protected from weather by a radome panel positioned directly in front of the radar. In this case, however, the antenna is embedded in a lossless material having µr ≈ 1 and ǫr = 2, and the radome panel is to be placed betwe...
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given by η2 = η0 √ǫr ⇒ ǫr = (η0 η2 )2 ∼= 1.41 (5.83) The phase velocity in the slab will be vp = c√ǫr ∼= 3 × 108 m/s√ 1.41 ∼ = 2 .53 × 108 m/s (5.84) so the wavelength in the slab is λ2 = vp f ∼ = 2.53 × 108 m/s 60 × 109 Hz ∼ = 4 .20 mm (5.85)
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5.4. PROP AGA TION OF A UNIFORM PLANE W A VE IN AN ARBITRAR Y DIRECTION 67 Thus, the minimum possible thickness of the radome panel is d= λ2/4 ∼= 1.05 mm, and the relati ve permittivity of the radome panel must be ǫr ∼= 1.41. Additional Reading: • “Radome” on Wikipedia. 5.4 Propagation of a Uniform Plane W ave in an Ar...
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in the +ˆz direction through simple lossless media. Note that electric field intensity vector is linearly polarized in a direction parallel to ˆx. Depending on the position in space (and, for the physical time-domain waveform, time), ˜E points either in the +ˆx direction or the −ˆx direction. Let us be a bit more specifi...
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68 CHAPTER 5. W A VE REFLECTION AND TRANSMISSION c⃝ C. W ang CC BY -SA 4.0 Figure 5.5: The same plane wave described in a ro- tated coordinate system, yielding Equation 5.87. c⃝ C. W ang CC BY -SA 4.0 Figure 5.6: The same plane wave described in yet an- other rotation of the coordinate system, yielding Equa- tion 5.88....
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changed. Let us now rotate the +zaxis of the coordinate system around the xaxis into the position originally occupied by the −zaxis. Now the very same wave is expressed as ˜E = + ˆyE0e+jβz (5.88) This is illustrated in Figure 5.6. At first glance, it appears that the direction of propagation has reversed; but, again, it...
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Cartesian coordinate system. One situation in which we face this complication is when the wave is obliquely incident on a surface. In this case, it is impossible to select a single orientation of the coordinate system in which the directions of propagation, reference polarization, and surface normal can all be describe...
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characteristics of the wave, as opposed to being determined arbitrarily and separately from the characteristics of the wave. The ray-fixed representation of a uniform plane wave is: ˜E(r) = ˆeE0e−jk·r (5.89) This is illustrated in Figure 5.7. In this representation, r is the position at which ˜E is evaluated, ˆe is the ...
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5.4. PROP AGA TION OF A UNIFORM PLANE W A VE IN AN ARBITRAR Y DIRECTION 69 Thus, k · r = βz, as expected. In ray-fixed coordinates, a wave can be represented by one – and only one – expression, which is the same expression regardless of the orientation of the “global” coordinate system. Moreover, only two basis directio...
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ky ≜ βˆk · ˆy (5.94) kz ≜ βˆk · ˆz (5.95) Then, k · r = kxx+ kyy+ kzz (5.96) With this expression in hand, Equation 5.89 may be rewritten as: ˜E = ˆeE0e−jkxxe−jky ye−jkz z (5.97) If desired, one can similarly decompose ˆe into its Cartesian components as follows: ˆe = ( ˆe · ˆx) ˆx + (ˆe · ˆy) ˆy + (ˆe · ˆz) ˆz (5.98) ...
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Propagating away from the z-axis means ˆk = ˆx cos φ+ ˆy sin φ (5.99) where φindicates the specific direction of propagation. For example, φ= 0 yields ˆk = + ˆx, φ= π/2 yields ˆk = + ˆy, and so on. Therefore, k ≜ βˆk = β(ˆx cos φ+ ˆy sin φ) (5.100) For completeness, note that the following factor appears in the phase-de...
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70 CHAPTER 5. W A VE REFLECTION AND TRANSMISSION 5.5 Decomposition of a W ave into TE and TM Components [m0166] A broad range of problems in electromagnetics in volve scattering of a plane wave by a planar boundary between dissimilar media. Section 5.1 (“Plane W aves at Normal Incidence on a Planar Boundary Between Los...
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added complexity is easily handled if we take the effort to represent the incident wave as the sum of two waves having particular polarizations. These polarizations are referred to as transverse electric (TE) and transverse magnetic (TM). This section describes these polarizations and the method for decomposition of a ...
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propagation ( ˆki) lie. The TE-TM decomposition consists of finding the components of the electric and magnetic fields which are perpendicular (“transverse”) to the plane of incidence. Of the two possible directions that are perpendicular to the plane of incidence, we choose ˆe⊥, defined as shown in Figure 5.8. From the fi...
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in the new , ray-fixed coordinate system. W e begin with the following phasor representation of the electric field intensity: ˜Ei = ˆeiEi 0e−jki·r (5.105) where ˆei is a unit vector indicating the reference polarization, Ei 0 is a complex-valued scalar, and r is a vector indicating the position at which ˜Ei is evaluated....
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5.5. DECOMPOSITION OF A W A VE INTO TE AND TM COMPONENTS 71 The electric field vector is always perpendicular to the direction of propagation, so ˆei · ˆki = 0. This leaves: ˆei = (ˆei · ˆe⊥ )ˆe⊥ + ( ˆei · ˆei ∥ ) ˆei ∥ (5.107) Substituting this expression into Equation 5.105, we obtain: ˜Ei = ˆe⊥Ei TEe−jki·r + ˆei ∥ Ei...
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apparent since the magnetic field vector is perpendicular to both the direction of propagation and the electric field vector. Summarizing: The TE component is the component for which ˜Ei is perpendicular to the plane of incidence. The TM component is the component for which ˜Hi is perpendicular to the plane of incidence;...
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whereas direct analysis of the scattering of arbitrarily-polarized waves is relatively difficult. Note that the nomenclature “TE” and “TM” is commonly but not universally used. Sometimes “TE” is referred to as “perpendicular” polarization, indicated using the subscript “⊥ ” or “s” (short for senkrecht, German for “perpe...
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of the field, and similarly the wave inside a waveguide may consist of multiple unique TM modes which collectively comprise the TM component of the field. Finally , consider what happens when a plane wave is normally-incident upon the boundary; i.e., when ˆki = −ˆn. In this case, Equation 5.103 indicates that ˆe⊥ = 0, so...
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72 CHAPTER 5. W A VE REFLECTION AND TRANSMISSION 5.6 Plane W aves at Oblique Incidence on a Planar Boundary: TE Case [m0167] In this section, we consider the problem of reflection and transmission from a planar boundary between semi-infinite media for a transverse electric (TE) uniform plane wave. Before attempting this ...
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Region 1. The electric field intensity ˜Ei TE of this wave is given by ˜Ei TE(r) = ˆyEi TEe−jki·r (5.111) In this expression, r is the position at which ˜Ei TE is evaluated, and ki = ˆkiβ1 (5.112) c⃝ C. W ang CC BY -SA 4.0 Figure 5.9: A TE uniform plane wave obliquely inci- dent on the planar boundary between two semi-i...
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reflected and transmitted components of the electric field will have the same polarization as that of the incident electric field. This is because there is nothing present in the problem that could account for a change in polarization. Thus, the reflected and transmitted fields will also be TE. Therefore, we postulate the f...
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propagation constant in Region 2. At this point, the unknowns in this problem are the constants Band C, as well as the directions ˆkr and ˆkt. W e may establish a relationship between Ei TE, B, and Cby application of boundary conditions at z= 0. First, recall that the tangential component of the total electric field int...
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5.6. PLANE W A VES A T OBLIQUE INCIDENCE ON A PLANAR BOUNDAR Y : TE CASE 73 total field in Region 1 is the sum of incident and reflected fields, so ˜E1(r) = ˜Ei TE(r) + ˜Er(r) (5.117) The total field in Region 2 is simply ˜E2(r) = ˜Et(r) (5.118) Next, note that all electric field components are already tangent to the bounda...
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boundary , it must be true that ki · r0 = kr · r0 = kt · r0 (5.122) Essentially , we are requiring the phases of each field in Regions 1 and 2 to be matched at every point along the boundary . Any other choice will result in a violation of boundary conditions at some point along the boundary . This phase matching criter...
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netic field components associated with the TE electric field components shown in Figure 5.9. obtained by applying the appropriate boundary conditions to the magnetic field. The magnetic field associated with each of the electric field components is identified in Figure 5.10. Note the orientations of the magnetic field vectors...
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Thus: ˜Hi(r) = (ˆz sin ψi − ˆx cos ψi)Ei TE η1 e−jki·r (5.126) Similarly , we determine that the reflected magnetic field has the form: ˜Hr(r) = 1 η1 ˆkr × ˜Er (5.127)
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74 CHAPTER 5. W A VE REFLECTION AND TRANSMISSION In the global coordinate system: ˆkr = ˆx sin ψr − ˆz cos ψr (5.128) Thus: ˜Hr(r) = ( ˆz sin ψr + ˆx cos ψr) B η1 e−jkr ·r (5.129) The transmitted magnetic field has the form: ˜Ht(r) = 1 η2 ˆkt × ˜Et (5.130) In the global coordinate system: ˆkt = ˆx sin ψt + ˆz cos ψt (5....
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where “ ˆx·” selects the component of the magnetic field that is tangent to the boundary . Evaluating this expression, we obtain: − ( cos ψi)Ei TE η1 e−jki·r0 + ( cos ψr) B η1 e−jkr ·r0 = − ( cos ψt)C η2 e−jkt·r0 (5.136) No w employing the phase matching condition expressed in Equation 5.122, we find: − ( cos ψi)Ei TE η1...
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follows: B = Γ TEEi TE (5.140) where Γ TE ≜ η2 cos ψi − η1 cos ψt η2 cos ψr + η1 cos ψt (5.141) It is worth noting that Equation 5.141 becomes the reflection coefficient for normal (TEM) incidence when ψi = ψr = ψt = 0, as expected. Returning to Equation 5.123, we now find C = (1 + Γ TE) Ei TE (5.142) Let us now summarize...
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5.6. PLANE W A VES A T OBLIQUE INCIDENCE ON A PLANAR BOUNDAR Y : TE CASE 75 simply state the result, and in Section 5.8 we shall perform this part of the derivation in detail and with greater attention to the implications. One finds: ψr = ψi (5.145) and ψt = arcsin (β1 β2 sin ψi ) (5.146) Equation 5.145 is the unsurpris...
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finding of this section: The electric field reflection coefficient for oblique TE incidence, Γ TE, is given by Equation 5.147. The following example demonstrates the utility of this result. Example 5.7. Po wer transmission at an air-to-glass interface (TE case). Figure 5.11 illustrates a TE plane wave incident from air ont...
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air to glass. η2 ≈ η0√ 2.1 ∼= 260 .0 Ω (glass) (5.149) ψi = 30 ◦ (5.150) Note β1 β2 ≈ ω√µ0ǫ0 ω√µ0 · 2.1ǫ0 ∼ = 0.690 (5.151) so ψt = arcsin (β1 β2 sin ψi ) ∼ = 20 .2◦ (5.152) Now substituting these values into Equation 5.147, we obtain Γ TE ∼= −0.2220 (5.153) Subsequently , the fraction of power reflected relative to po...
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76 CHAPTER 5. W A VE REFLECTION AND TRANSMISSION 5.7 Plane W aves at Oblique Incidence on a Planar Boundary: TM Case [m0164] In this section, we consider the problem of reflection and transmission from a planar boundary between semi-infinite media for a transverse magnetic (TM) uniform plane wave. Before attempting this ...
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z= 0 plane. The wave is incident from Region 1. The magnetic field intensity ˜Hi TM of this wave is given by ˜Hi TM(r) = ˆyHi TMe−jki·r (5.154) In this expression, r is the position at which ˜Hi TM is c⃝ C. W ang CC BY -SA 4.0 Figure 5.12: A TM uniform plane wave obliquely incident on the planar boundary between two sem...
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reflected and transmitted components of the magnetic field will have the same polarization as that of the incident electric field. This is because there is nothing present in the problem that could account for a change in polarization. Thus, the reflected and transmitted fields will also be TM. So we postulate the following...
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specific convention, and will be incorrect with respect to the opposite convention. W e choose −ˆy because it has a particular advantage which we shall point out at the end of this section. Continuing, we postulate the following expression for the transmitted wave: ˜Ht(r) = ˆyCe−jkt·r (5.158) where Cis an unknown, possi...
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5.7. PLANE W A VES A T OBLIQUE INCIDENCE ON A PLANAR BOUNDAR Y : TM CASE 77 where ˆkt is the unit vector indicating the direction of propagation and β2 = ω√µ2ǫ2 is the phase propagation constant in Region 2. At this point, the unknowns in this problem are the constants Band C, as well as the unknown directions ˆkr and ...
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˜H2(r) = ˜Ht(r) (5.161) Also, we note that all magnetic field components are already tangent to the boundary . Thus, continuity of the tangential component of the magnetic field across the boundary requires ˜H1(r0) = ˜H2(r0), where r0 ≜ ˆxx+ ˆyysince z= 0 on the boundary . Therefore, ˜Hi TM(r0) + ˜Hr(r0) = ˜Ht(r0) (5.162...
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the boundary . This expression allows us to solve for the directions of propagation of the reflected and transmitted fields, which we shall do later. Our priority for now shall be to solve for the coefficients Band C. Enforcing Equation 5.165, we observe that Equation 5.164 reduces to: Hi TM − B = C (5.166) A second equat...
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propagation. Expressions for each of the electric field components is determined formally below . From the plane wave relationships, we determine that the incident electric field intensity is ˜Ei(r) = −η1 ˆki × ˜Hi TM (5.167) where η1 = √ µ1/ǫ1 is the wave impedance in Region 1. T o make progress requires that we express...
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78 CHAPTER 5. W A VE REFLECTION AND TRANSMISSION The transmitted magnetic field has the form: ˜Et(r) = −η2 ˆkt × ˜Ht (5.173) In the global coordinate system: ˆkt = ˆx sin ψt + ˆz cos ψt (5.174) Thus: ˜Et(r) = (ˆx cos ψt − ˆz sin ψt) η2Ce−jkt·r (5.175) The total electric field in Region 1 is the sum of incident and reflect...
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= + ( cos ψt) η2Ce−jkt·r0 (5.179) Now employing the “phase matching” condition expressed in Equation 5.165, we find: + ( cos ψi) η1Hi TM + (cos ψr) η1B = + ( cos ψt) η2C (5.180) Equations 5.166 and 5.180 comprise a linear system of equations with unknowns Band C. This system of equations is easily solved for Bas follows...
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TM ≜ η1Hi TM in Equation 5.169, yielding: ˜Ei(r) = (ˆx cos ψi − ˆz sin ψi) Ei TMe−jki·r (5.185) The factor η1Bin Equation 5.172 becomes Γ TMEi TM, so we obtain: ˜Er(r) = ( ˆx cos ψr + ˆz sin ψr) · Γ TMEi TMe−jkr ·r (5.186) Thus, we see Γ TM is the reflection coefficient for the electric field intensity . Returning to Equa...
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5.7. PLANE W A VES A T OBLIQUE INCIDENCE ON A PLANAR BOUNDAR Y : TM CASE 79 can be found using Equation 5.165. Here we shall simply state the result, and in Section 5.8 we shall perform this part of the derivation in detail and with greater attention to the implications. One finds: ψr = ψi (5.189) i.e., angle of reflecti...
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reflection coefficient for normal (TEM) incidence when ψi = ψt = 0. If we had chosen +ˆy as the reference polarization for Hr, we would have instead obtained an expression for Γ TM that has the opposite sign for TEM incidence. 3 There is nothing wrong with this answer, but it is awkward to have different values of the re...
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Thus, we obtain what is perhaps the most important finding of this section: The electric field reflection coefficient for oblique TM incidence, Γ TM, is given by Equation 5.191. 3 Obtaining this result is an excellent way for the student to con- firm their understanding of the derivation presented in this section. The follo...
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Equation 5.191. Calculating the quantities that enter into this expression: η1 ≈ η0 ∼= 376.7 Ω (air) (5.192) η2 ≈ η0 √ 2.1 ∼ = 260 .0 Ω (glass) (5.193) ψi = 30 ◦ (5.194) Note β1 β2 ≈ ω√µ0ǫ0 ω√µ0 · 2.1ǫ0 ∼ = 0.690 (5.195) so ψt = arcsin (β1 β2 sin ψi ) ∼ = 20 .2◦ (5.196) Now substituting these values into Equation 5.1...
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80 CHAPTER 5. W A VE REFLECTION AND TRANSMISSION c⃝ C. W ang CC BY -SA 4.0 Figure 5.13: A TM uniform plane wave incident from air to glass. |Γ TM|2 ∼= 0 .021; i.e., about 2.1% . 1 − |Γ T M|2 ∼ = 97.9% of the power is transmitted into the glass. Note that the result obtained in the preceding example is different from th...
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Let a point on the boundary be represented as the position vector r0 = ˆxx+ ˆyy (5.198) In both Sections 5.6 (“Plane W aves at Oblique Incidence on a Planar Boundary: TE Case”) and 5.7 (“Plane W aves at Oblique Incidence on a Planar Boundary: TM Case”), it is found that ki · r0 = kr · r0 = kt · r0 (5.199) In this expre...
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5.8. ANGLES OF REFLECTION AND REFRACTION 81 respectively; and β1 and β2 are the phase propagation constants in Region 1 (from which the wave is incident) and Region 2, respectively . Equation 5.199 is essentially a boundary condition that enforces continuity of the phase of the electric and magnetic fields across the bo...
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Therefore, we may express Equation 5.199 in the following form β1 (ˆx sin ψi + ˆz cos ψi) · (ˆxx+ ˆyy) = β1 (ˆx sin ψr − ˆz cos ψr) · (ˆxx+ ˆyy) = β2 (ˆx sin ψt + ˆz cos ψt) · (ˆxx+ ˆyy) (5.206) which reduces to β1 sin ψi = β1 sin ψr = β2 sin ψt (5.207) Examining the first and second terms of Equation 5.207, and noting ...
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of the relative values of constitutive parameters; i.e., µ1 = µr1µ0, ǫ1 = ǫr1ǫ0, µ2 = µr2µ0, and ǫ2 = ǫr2ǫ0. In terms of the relative parameters: √ µr1ǫr1 sin ψi = √µr2ǫr2 sin ψt (5.211) This is known as Snell’s law or the law of refraction. Refraction is simply transmission with the result that the direction of propag...
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