Solution Manual for Fundamentals of Electromagnetics for Electrical and Computer Engineering, 1st Edition
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Solution Manual for Fundamentals of Electromagnetics for Electrical and Computer Engineering Nannapaneni Narayana Rao Edward C. Jordan Professor Emeritus of Electrical and Computer Engineering University of Illinois at Urbana-Champaign, USA Distinguished Amrita Professor of Engineering Amrita Vishwa Vidyapeetham (Amrita University), India
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CONTENTS CRaPLEr 1 covvn iii eee] CRAPLET 2 Levies een 1S Chapter 3... eee 29) Chapter 4 Lo... eee A Chapter 5 .......oiiiiiiii ie DO) CRAPLEr 6 Levee en 82 Chapter 7 ........oiiiiiiiin iin 104 CHAPLET 8 vivitar. 134 CRAPLEL 9 vise eee eccrine 153 Chapter 10 ......ouviiiiiiiiiiiiiie cee LTO APPENAIX A Louies eee 183) Appendix B o.oo. UBT
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CHAPTER 1 1.1 (a) Total distance = 1 + ++ Lod =om wr T2727: 1-45" (b) Distance north = [—+ += —=—L_ =0.8m Tae 1+y A 11 1 1, 1.1 Distance east = a (ae =04m .~. Final position is (0.8, 0.4) (c) Straight line distance = +/(0.8)2 + (0.4)? = 0.8944 m 1.2. A+B+C=2a;+3a+2a3 — (1) 2A +B-C=a; + 3a, —(2) A-2B+3C=4a +50, +a; —(3) (1) +2) — 3A +2B=3a; + 16a, + 2a; — (4) 2)x3+(3)— TA +B =Ta, + lday +a; — (5) [G)X2-(@)] +11 >A=a,+2a, — (6) 5)- (6) x7 — B=a; —( H=-©)-N— C=a +a +a; — (8) 13. (A+B)*(A-B)=A*A-A+*B+B*A-B+B=A*—B (A+B)Xx(A-B)=AXA-AXB+BXA-BXxB=2BxA For A = 3a; — 5a; + 4a; and B = a; + a, — 2as, A +B =4a; — 4a; + 2a;, A — B = 2a; — 6a; + 6as, A’=9+25+16=50, and B*=1+1+4=6 A+B)» (A-B)=8+24+12=44=4>-pB 1 — StudyXY
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a, a, a, (A+B)x(A-B)=|4 -4 2|=-12a,-20a,-16a, 2 6 6 a, a, a, =2|1 1 -2=2BxA 3 5 4 14. Bx C=-4a,+2a,+ 8a, Ax (BxC)=8a,+16a, CxA=-a,-2a,+7a, Bx(CxA)=-12a,-8a,—4a, A xB =a, + 2a, + 3a,, C x (A x B) = 4a, — 8a, + 4a, AxBXC)+Bx(CxA)+Cx(AxB)=0 In fact, this quantity is zero for any A, B, and C. 15. Arca= SABsinc = Lia XB| 2 "2 For the points (1, 2, 1), (3,4, 5), . 8 and (2, -1,-3), 7 B sind A =4a, + 6a, — 4a, B = 5a, + 3a, — 8a, A) A xB =-36a, + 12a, - 18a, ‘ 2 Area = ze? +(12)*+(~18)* =21 units. 1.6. Area of the base = [B Xx | ; Height of parallelepiped = Projection Es = of A onto the normal to the base A [E] ZA. BxC B [BxC]| +. Volume of parallelepiped = Area of base x height =A « Bx C For A =4a,, B=2a, +a, + 3a, and C=2a,+ 6a, A*BxC=0. Hence, volume of the parallelepiped is zero. The three vectors lie in a plane. 2 — StudyXY
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1.7. The vector A must be perpendicular to both (a, + 2a,) and (a, — 2a,). Hence A = C(-a, + 2a,) X (a, —2a;) = C(2a, + 2a, + a,) where C is a constant. To find C, we note that a, Xx A = a, X C(2a, + 2a, +a,) = 2a, — a, C=1and A =2a, + 2a, +a, Verification: a, x A = a, X (2a, + 2a; + a) = a, — 2a. 1.8. Vector from A(S, 0, 3) to B(3, 3, 2) = 2a, + 3a, — a, Vector from C(6, 2, 4) to D(3, 3, 6) = 3a, + a, + 2a, CD 6+3-2 Component of AB along CD = AB + —— = ————= = 1.8708 P € CD J9+1+4 1.9. Writing the equation for the plane as = 5 tog =1, we find the intercepts on the x, y, and z-axes to be at 15, -12, and 20, respectively. Thus 3 Rup =-15a,— 12a, : foo Rac =-15a, + 20a, ) Rac x Rap = 240a, — 300a, + 180a, < 2 , a= Ryo xR yp _da 5, +3a, As Rac XR gp 572 x . Distance from origin to the plane = 15a, * a, = 2 . 1.10. For y = 2x, z = 4y, we have dy = 2 dx, dz =4 dy = 8 dx. sod =dea+dya,+dza;=dra,+2dxa,+8dxa, = (a, + 2a, + 8a,) dx, independent of the point. 1.11. For x = y = 7%, we have dx = dy = 27 dz. At the point (4, 4,2), dx=dy=4dz sod =dva,+dyay+dza;=4dza, +4 dzay+dza, = (4a, + 4a, + a,) dz 3 — StudyXY
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1.12. Differential length vector having projection dy a, = dy a, dy . . . i. Differential length vector having xe yer / ik 3x : projection dx a, is J Sai pat 1 [dx % [07 dxay+dza;=doac— 5 da, t L rey a = (a “3a J dx, 4 since forx +2z=2,dz=— : dx, independent of the point. . _ 1 1 sds = a, ~5a; dx Xdya, = Fata, dx dy. 1.13. One vector tangential to the ¥ surface is dz a,. Another tangential vector is given by dl =dxa,+dya, 14 2,4, = dra, +2xdxa, @*) = (a, + 4a,) dx ld .~. Vector normal to the plane = (a, + 4a,) dx X dz a, = (4a, —a,) dx dz Unit vect 1 to the pl fa, nit vector normal to the plane = ——==. ? 7 1.14. Denoting K(x, y) to be the height field, we have Pry +r =4, 7+) <4 or, h= \J4=x2~y2 FP +y <4. 1.15. The number field is x +y + z. .~. Constant magnitude surfaces are the planes x + y + z = constant. 4 — StudyXY
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1.16. d(x, y, 2) = xa, + ya, + za, Constant magnitude surfaces are x” + y* + z* = constant, and hence are spherical surfaces centered at the corner. Direction lines are radial lines emanating from the corner. 1.17. v = —rwsin ga, + rwcos ga, = aX-ya, + xa,) Y N 9 1.18. f(z,1) =10cos (27 x10't ~ 0.1 77) 1 CUNY aro! t=0 kzLix0 E: id t= Fa t=gxto (® : — Sar Ve SSCS AAV AN a SCO > 320 322-5 3=5 3=1S 310 ’ wi os HZ WT SON . 4 Te >> <> f(z, 1) represents a traveling wave progressing with time in the positive z-direction. 5 + StudyXY
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1.19. f(z,1) =10cos (27 x10" +0.1 72) 1 1 1 -1 felix k=2x6 bly EzixkG t=0 § z 3 € 3 © ~ RY MN VO) Ll BRN SN . CONN - ARR E TOS << >> : zlo 27.6 =5 22.5 3=0 w 3 PVN VL TY OY TION TSS IN COON B= <> - f(z, ©) represents a traveling wave progressing with time in the negative z-direction. 1.20. f(z, £) =10cos 272 x 10'¢ cos 0.1 72 t=0 = : , exe” “ fi SEIN 0 Bs — — > 0 Thm =7.01 Tez2 xd” | “te Seas xe . 5 - ® Cem 7.01 Pa Se TN + % -1.07 {yztbm “10 Kaz iom A f(z, 1) represents a standing wave. 6
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1.21. (a) The two components are in phase; hence, linear polarization. (b) The two components are perpendicular in direction, differ in phase by 90° and equal in amplitude; hence, circular polarization. (c) The two components are perpendicular in direction, differ in phase by 90° but unequal in amplitude; hence elliptical polarization. 1.22. F; and F; differ in phase by 90°. 1.3 . . | =+/3+1 coswt = 2cos ar; [Fy = FREE sin wt = 2sin wt . i .. Fy and F; are equal in amplitude. FF, = BLL =0. .. Fy is perpendicular to Fs. Thus Fy + F; is circularly polarized. 1.23. \ [ ~ | H EN H Ly SE Co The polarization is elliptical with major axis in the y-direction, minor axis in the x-direction, and eccentricity equal to V2. 1.24. 10 cos (ax — 30°) + 10 cos (ax + 210°) Iw | l 10 7” + 10M” =10 30° 500” Re .~. The sum is 10 cos (ax — 90°) = 10 sin ar. ~~. ad 1.25. 3 cos (ax + 60°) — 4 cos (ax + 150°) Yor be Im J 3e = de SEAN og J60°-53.13) _ £ , j68T 360 60° s =5e =5e Fa Re — 5 cos (ax + 6.87°). £803 7 — StudyXY
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1.26. Replacing z by 710°7 i by I, and 13 cos 10% by 13¢/, we have 51070 x j10°T +127 =13¢/" GT =13,T=0 1B mer or, (12+ j5)I =13,1 = 25 WET =le Thus i= 1 cos (10% - 22.62°) =1cos (10% — 0.1267) 1.27. From the construction shown, 0 —= mg =tan45°=1 [3 © El o& 2oN — FR, or, Q =1 87 £91 mg 470,20 Vo VEL Q m3 1.28. (a) At the point (0, 0, 100), I x 476499) 47g, (101) Q . 1 __0 107-99" iN 7 47g) 99% 1012 ° x 0 (100+1)%-(100- 1)? Q 400 YT arrvey seppeey Ll ps pL 475 (100-1)% x (100 +1 Eo (100% —1) 400 EEL By, 47€) 100 100% 78, (b) At the point (100, 0, 0) 20 1 E=————————>a 478, (1007 +12)¥2 °F A 2760(100%) 8 — StudyXY
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129. E= Q |a,+2a,+2a, LAA, +2, LAAs, ta, 47g, 93/2 932 932 a +a, +2a, 2a,+a, +a, a,+2a,+a, tear Tar TT en Laat, 2a, Lata, ta, 1232 332 =< S42 Lo (a, +a, +a;) dm 3 (or Why WBC ——£ (0.18519+0.27217+0.04811+0.19245)(a +a, +a,) Xx y Zz 47g, 0.0555 Q = ata +a,)N/C. 1.30. For the ith segment, . -3 kd z= 2-1 and charge = EU C. if 100 50 __L FR" 50 Cpe 2 N07 1 ¥ - =a 2% PREY y Eh (2 +1) 50 107° a. a TZ - “Ta 2.10 (2i-1 +1] a, i yy _2i-1 os 2i-1 1.31. For the ith segment, z = 100 , charge density = 10 100 C/m, . 6 and charge = 107° Kami BX = 10 @i-y C. 50 6. Cpl 2 10°°2i-1) 1 SB) 5 2 372 i=1 (2 +1) 7 50 107’ . Ly a TY? = 2,010 @i-1) +1] a, [= 9 — StudyXY
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1.32. Dividing the circular ring into n segments and using the symmetry of the field about the z-axis, we obtain _ ¥ x 22(2)%107° 1 B=) im a p (2 +1 ) 1 _4mx107 008944x107 Came & ‘ 4 =1.012x10"a, NIC. Xx 1.33. For the (i/)th area, C2i-1 _2j-1 ¥ *= Tao 7 100M charge = —— x10 =4x10°77C J 10000 Wa ITLL: y 4 S& axa” ii - Ee NN Ea, [ATT 77TT AE Led Led (i 4 2 4 1)Y? 3 i=l j=l x _7 50 50 _ 4x10” RTA I i “mm 2210 @i-D*+107*@2j-1) +1] a, i=l j= 2i-1 2j—- 1.34. For the (i/)th area, x= Soy = us, 2-1) 2j-1Y charge density = 107 (G35) =107°(2i-1)2j-1)* ¢/m? _ 4 TT I “130: yin 1\2 charge = Joes X10” 2i-1)(2j 1)? =4x107°@i- D2) -1) C ped Shyer ner, 47g pg +? +1)? : i. 50 50 _4x107? Qi-12j-1)? AT pe [10 Qi-12 +1072) -1) +1] 10 — StudyXY
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Ne? . 1.35. (a) J = Nev= — Ey sin ax a, maw 12 2.10738 = MOT XLOREXI0 10 sin 2m x10’ a, 9.1083x1077" x 27 x10 =0.4485%x 10 sin 27x 107 a, A/m? (b) AI =J + AS = 0.4485 x 10 sin 27 x10" a, +0.01 (a, +a) =0.4485x 108 sin 27 x 107 A 1.36. Denoting x to be the displacement, we write the equation of motion to be 2 mE = mg kx + gE cos ax l dr ym 2 E, cos wt dx on m=z + kx = mg + qEo cos at 9 t The steady state solution consists of two parts. One is x = = due to mg. To find the second part x, we write (je) mx, + ky = qEge’®, or, (k —a&’m)%, = gE, = = 15 mg 4k X) =——5—. Thus x = x +x, = —>+—"—>— cos wx ? k-a’m TR k-a’m . dx qEyw Velocity = — = ————— sin wr Yd k-a'm I, dya,X(-a 1.37. dF, =I; dxa, x Hela da, x(Ca,) 47(l) ¥ =0 I,dysy I dxa_ xa, . 1 : Fy =I, ya, x| LL 1xEy 47(l) * - Ho Ho =1, dy a,x dxa, =z la dxdya, 11 — StudyXY
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-a, +a, +a 1.38. (2) For 0, 1, 1), ag = ——2—"% R=4/3, and 3 pote! dx (a, +2a, t2) (a, +a, +a,) ar 3 Ne to I dx =——=—(-a,+a,) of Ch (b) For (2, 2,2) acta, +24, R=3,and or (2,2,2),ag= ——7=——,R=3,an * Nd pot! dx@,+2a,+2,) (a,+2,+2%,) 4 9 3 =0 1.39. (a) At (0,0, 1), the components of B M perpendicular to the z-axis cancel, 1 whereas the z components add. Thus Be1 Hg 0012, X (0.00%, +a) a TY 4 (140.0052)? a “ 5%107 - [2 000005, £0012, a, “22H, (b) At the point (0, 1, 0), poto|__ 001 a+ 0.01 a, 47] (1-0.005) (140.005) N 0.0la, X(=0.005a, +a) B 0.0la, x (0.005a, +a.) (1+0.005%)? (1+0.005%)7? Ho | 0.01x4x1x0.005 2x0.01x0.005 7 EP I Sa Sno I TE Az (1-0.005%) (1+0.0052) 107%, TTT 12 — StudyXY
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1 1.40. For the ith element, dl = 30% N .\2 kd 2i-1 R= (5%) a" ~ R _1 2i-1 i ag =| a, ~| Tog Jaz |» an I tl 1 (EA), | L x AB =r 505% Too J | 7 Al 2007R 50 io] 50 J" = —_ —4 [ — B=2)" dB 20> [1410 @i-1) ] a, i=l i=1 1.41. Dividing the loop into n segments and using the symmetry of the field 3 about the z-axis, we obtain ol 222) 2 g B= —— a : 32 “2 Dir n (2422) y _ 8mul _ * = Ins =0.179l a, 1.42. Equating the magnetic force to the centripetal force, we have 2 . my my evBy = — on r= By PR e room v . _ oo _ eB Orbital frequency = 5 = om For By =5x107, 13 — StudyXY
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