Solution Manual For Theory Of Vibrations With Applications, 5th Edition
- Mechanical Engineering
- 458 pages
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Solutions Manual-Theory of Vibration with Applications by William T. Thomson and Marie Dillon Dahleh TABLE OF CONTENTS CHAPTER 1 1 CHAPTER 2 9 CHAPTER 3 41 CHAPTER 4 76 CHAPTER 5 116 CHAPTER 6 149 CHAPTER 7 178 CHAPTER 8 201 CHAPTER 9 229 CHAPTER 10 249 CHAPTER 11 350 CHAPTER 12 366 CHAPTER 13 412 CHAPTER 14 438
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yi 2 = A su Ot A= 0.20 ce Y=o0.i5s Da ZW _ a/.89 Ms 7 L = WA cos wit x = WA = 8.35 Omi . Pred es nda x == A sow JE X may = DA = 350.7 om/s2 -_ Tm Tr = : - Wa 2Tf =27xgz2=5152"% WW = 0.2655 x 10 2 = 980.9 <m/s2 x, = % Wr = 50x 980.4 _ , seq wr = Fr Gacssx 106 TOE om - oo / —-3 D=2Tf = 2x0 = 62.83 2; Y= £ = 0.10 s Fay = DA = 4.57 mp A= 0.07274 m = 7.274 cm Koay = SA = 287.7 mss - d= 4 % = Asta, t tsaat) = 24 ca f(a) “Sot (ag rel, ) let w,= 0, Wom WAL, Qa, =2D044DF 20 sox FT 2A cost AE - sant -_ / —5 is 5 i Z=4+3. = 5(wmo+isdug)=5e re’ <) 6= tas = 3°52" = 0.¢435 & 4 -- L=6 =-6 ‘oe : z=4Ae A =7¢*+ 2% 2 6.325 2+3¢ 4 = ¢ _ -7 °o Sum = ¢ +2C 0 Tw2 = 7/872 = 032/17 : z =c.325 ¢ OT 12 ew = 6.325 [/8°2¢’ A ! + StudyXxy
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, z= A (cme + < snp)=Ae’ z “ . . . / cz=A(iCme ~Same) = Z, ° z 0 A =Alea(o+ 90) + Csi (6+90)] ® 1-8 Z=30° R . A * R =5+4cos30"=5+3.47 ’ 4 CP = 8.47 4 ; R = 45m 30° = 2.00 Var At R=) 847% 2.54 = 8.70 6 = tan” 2 = 12°57 £=9 id X(t) is odd Function i GuzO % t b, = # [rarcmmat 4 “% = 5 < = 27 bor = Z 0 4, = | fensmmnt (— | 4 “ o Pe Cw mnt | _ emawt |B] a = =x on =F (1mm) iz o bh =f0 for m even ” = » m odd Kly< 2 (simu +f Smit + Fomsits os) 2 + StudyXxy
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L=i0 . . x(t) Z(E) is even function bu = 0 | il "owt Ks ou fmt | “% ar d r= pus Wz mw, -% +% ’ Tr a, = # Jeans dwt) «4 fer emme dtoy “4 Jem nt de = SA 7% rd —fr m= 3 7 4, --- 2) = 2% (cout -Fcasut +L emsut-o-) I= 1] ro a(t) & even function bozo L(t rm -Tx1s0 = > wi xe) =[# +7) wr Z(w-1) o<t sm fa, = average value = # ° Tr G, = £4 (t+m)casnutdiwt) + £3 (r-t)cos mast d(wt) - 0 kid = z [+ (r-t)cos maw, dlw,t) because of symmetry ° ats wt _ 2 sa + _ 2 (emmat wt sum mat =F = | 2, (moet rs <) o ° = [0 Hr nn even Ze for nn oda NCCT It £ wast NY, 3 + StudyXy
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I —i2 Lo x = = o0=< wits 2T Zz ot a imwt 27 c = wt oo g 97 = 3 ar © A [4 = vd c na He —enwlt p ime . » where on = wt € Wt) = L — [-en6-— rf ’ 49) or | Ee (- J o-ut o [2] = [- + (1+ ¢amm eo z 2 Tent mt J ]- rom ’ : (ut owt Lawt iz sat isu Pi ; ) ) 1 Gd ] COBRA 41 -e )+i(e ~e Get (e e Tr] . - Lg, a. 24 2 [shaf +f Smant vf Smut ] 7-1/3 wt Oo z Fat Ll Io = reo 2 le A x fd [4 set dt = Lm 4 [sm corer) ar o . 7 0 lm A(t Sm2at)|E A sel : Taw -3¢- PTX) ) sd (% or )= 4 2 eR CE EY re) £ wt) 2 Ll 6% ox gsan _ or 5 AT [A x* = L rot = L [L (4.5) =z) J o = t Loam — =L (amy. 4 = a ( 5) 3 4 + StudyXxy
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L=/4 cont FS. of saw tooth wave = 2) = 4 — F(semet + smart rd soswte--) whe) = L yore Ce . =) (¢) = 7 —F (smawt +f saw, ro: . J su 2 +45 (sw wt + 2 Sew ze tens) = —E (some Ea TA --2) ~ 2 - 2 .. cross products which c(t silt eee) + 0 infgeute to zero £ oo pr a T B 1 cosdwt r x(t = L Cosaw,t L_ coawt Cos 3a +f ) 2 * rar ’ AT ‘ *qmuT ‘ | ° ° o 0 Lo L(y sezwt)|T 1 L sgt (T rir tl wo) ap EE Fable o 0 Let WT =2T£& where #15 an Steer —> © rk VLR AC = a 1 L 4 Lr * Te a | <oas = dtm tian TE Gm o = -- A SERA CRF EE ) = 3 1 =15 —— Xt)=+% + =A (coset +4 cnt + LCST +-- 2) Fourier Spectrum = plot of Coefficients. For His case b =o Co=Yaitb: = am Ces § 5 405 -135 .08 -5 -4 -3 -2 -/ o 7 2 3 4+ 5 mm > + StudyXy
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[=e 2 “ #3 [2%4 a c= 2 = average value= AT £ =f a, =L senmbr = ol su mar = - = L (I- ex mam, b, =L ( csmbm) = L (1-cs pT) - T_T [rrr ad 2 Com Yar + 5. c= (7-22) 2 === mm [= Be mm Ca [2 / . 275% -é60° <4 c0689 —¢o0® z 1375 60° 5 0552 co 3 ° ° JA ° 0 Cu EN é. A: a ~ IN °o / z 3 4+ Ss ¢ ~ 2 3N aA 4=i7 Len —S = hemo + Leng £ Ling = nsand 5 — = 2) ” ind =[1-Gfs'e] ) - um 2 nE ton = 1-43 fords - 4 (35% Ss nli-emorg(f)sido f(s vo] using Sms = L(/-emz0) 3 some = £4 -20026 + {ens6) S=t[i-cne rE) cm20) 4 --- } ) = - —L/n _ which retains only =rnli+4(%) se £(3)en2e +---] ® to First power Ratio of 2h armonic S15 far monic =4(3) = 7% 6 + StudyXxy
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[=/8 T . KE = lim A A . A RY | gat * Too +f (dt > A . ° = 0./10A noms =) xz = 0.3/62 A - L=19 x = (1- Z) ost = 2. 2¢ 2 *= = s L, t= L i 2t * £ 20-2 Ea - 3 TE 1 —20 % - Db =20ly (F) = 0.50 % |. 0-50 _ lga(%)=%22 = 0.0250 * = 70 9°%° _ 0593 (3) Se = 4 %,=10593 % = 10593 x 2.5 mm = 2.6458/ Error = 0,0593X%X 2.5 py = 0.148 mm ma De sm bye) 20 Db = 20 log, (50) = 33.98 Db = 20 log, (100) = 40.0 ~~ x = Zp = Db = 20 go (3) = 32. ~ x ad = 32 L.(2,) = zo =/-¢0o % leo = = 1/0 = 39.8 1000
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| —- 23 PA | — = J = (-1)= 0 [— I oR ar Ta 8 a 1) Pe — - 25 oo J (2 FA C= JD = 00 (eld Fuckin) EYL (ICDL FO) = ED ever archon)
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2=l— EF 229 ro. 576 5.7 - 5.42 Hs Y 4 wm V7.57 = 2-2 ~ YE N fi NEA %- (kk) £ t LY% = [ZB [X 2 J = Z%5 1 = Xk oo ky =F Ek 4 frih ix BERT re a 2-3 14 t 2.2¢kg «4.53 ky. 2% iA = 0.455 m, 2.24 2 7 % =m) 2 = 2m [Aa Ke (Lf (5) 05 <4 xg83. = 883.5 N/m = 0.159 s 9 + StudyXxy
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2-4 2 _ x 24 \* * (am 77)* 2. (mf) = (2m 2) peor =(2 %7) mor 453 * , _ as = (2) am = 0.9028 Ag £ = 87.48 M/m 2Z=5 % measurca from static eguibibriam pasitiin of m, A k £q. of mation after impact "2 23 ny (reo) x = —Rx + ™, 3 IE + fx Gen Solution’ V pA 2(t)= ad 4 Asoo + Bomal x mg Ld condita: x2(0) = © = xd +B iB=-T x(o) = Tergh = wA vA = ™af2gk my 7m (mt me) GE —_ w= ] ~ ry cox) = Tad ow mylgh Yon pu z TBE Smt — 3 em wt = Tt (1- emwt) + mah ot e Yh(mro,) PE % = x, HWE + Sue WE = 2enzt — Sem 2¢ i = —45m2t —femat =0 lam2ia-2 So2t = 116.57° San 16.57.8944 nie. 5] = — 4472 Kppay = 2(-. 4472) — 4 (.7944) = —4.472 Cm Fora = SH, = 4(x4.472) = £17.59 em/s* 10 + StudyXY
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. . . 2-7 7,6 =-wne 5 = -we J. Wa o Tox o 15.83 A > T T2 rr GD) ) © Y SJ -HA = _70,¢" il J = Jp Fi = /5.83 ~ 300% Je = G.30 bon sec” I J 2-8 @ =m 82 = 555 nh = Wr 2/35 x.25% 5/76) ge A : 20.355 25%" m® = - 2 = 0.76) = FELLESE = 0.0356 % fy 2-9 Ro = Be Work dene = change in KE 2 2.2 +z zz | a= 2 w# Eh Ral ™ ! . | vertical displ = J= wu k= rad. of gyr. 20 ene =e[1=(1=F4)] 4 set ge) WaT. Wt” | 6 To z 2 I g = 2Y: = 2542 217 9.81 = .2032 « JE 27 1.829 = .4507 mm Shall A J 2-10 Moment about Shaft = (Stn) wr Simo [ET (T+ 58) § = - (ase) wr sin / ANG RES ? | ai YS NY z — (awsme) 6 ody / ‘ ro Ie / yes w Tur / Cm Taw Jr Yet / | j= pamlicl pfereicte planes / 7 + StudyXy
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2-0 I" 2 LL 7 = Fm - £# J, 6 6 = x _ FA .z . f(m + =) x = wx _ . i 7 _£ U = $42 GQ =) mr Gipt - TTT Crm 2-1/2 2 _ LC - ZF 2)" Tear) L= 3(5)=s5(E)= 0.9% m C =L(w8) = 903/75 ms 6 = =I 7a s820° - A 231 ct a 17h = 5, TZz=/3 a YY — Z=/3 water weighs F80L.M/m> PRIA 98012 TR, Ms busyant force = MA xp 2 mE = Sx Lo. x =) ~~ m = 0371 Ry wr BE 2m Tre 2 = .0032 m ~~ 0372 = a = . ! es 97 5 2-4 moment bout geo. center .. x -wge = J & = -0 J, 6 . Jo= gw gw U3) ae ww ° w? (afm) Zs TT . Ky —-wWhke =J6 = -2DJ6 y. J 5=Z = YZ = am f= [ETS pd r wh Z-1g Dispt. of <5 “Bid Tay = Um 2.2 ad «RE T= fmr-R)6L + # iy Omen As a a * A =f m[(e-A) + (RAY [Wek i = ~ - =X Unie = mg 7 (1-c6,,) 5 mga Ea 12 + StudyXxy
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2-16 cont Tay = Unies . Rg. _E_ WF ROR) Rr (RPE) 2R(R=F) IR(R-1) Fe AR . = YR(m-2) ak = but 7 = AE oo Team Z J 2-17 ~ 2 = Uz mgh(i-cng) 5 mghtd xp=ie 2 2 a2 _ £ [a6 |" = a” 6 sms E22) TEA ~ ERE ie Let T-g(mk)é" = $05)" . LyE Trang = Umer ERC a wre TE — ~ PE 4 ia FH For ly T-= 3 mp we L* e* . U="55%% Ar sam EE = LYE -h/L a #2 b= Sl [7 (£) em er 2-19 x wba 8 a wWab 6 b IM= JO == TET ww & wa wb ate a+b are wre s Wab gp =o b ta # “ ° § + (928 )e =0 t w x | i | wb as ( wt) , , lam ow N , Cop. L Y9eb ry > 10 .e ka amr Pal Plan View wa ra 4 . = 0 Zh 13 | T= StudyXY
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