{VERSION 3 0 "IBM INTEL NT" "3.0" } {USTYLETAB {CSTYLE "Maple Input" -1 0 "Courier" 0 1 255 0 0 1 0 1 0 0 1 0 0 0 0 }{CSTYLE "2D Math" -1 2 "Times" 0 1 0 0 0 0 0 0 2 0 0 0 0 0 0 }{CSTYLE "2D Comment" 2 18 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 } {CSTYLE "2D Output" 2 20 "" 0 1 0 0 255 1 0 0 0 0 0 0 0 0 0 }{CSTYLE " " -1 256 "" 0 1 0 0 0 0 1 0 0 0 0 0 0 0 0 }{CSTYLE "" -1 257 "" 0 1 0 0 0 0 1 0 0 0 0 0 0 0 0 }{PSTYLE "Normal" -1 0 1 {CSTYLE "" -1 -1 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 }0 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 } {PSTYLE "Heading 1" 0 3 1 {CSTYLE "" -1 -1 "" 1 18 0 0 0 0 0 1 0 0 0 0 0 0 0 }1 0 0 0 8 4 0 0 0 0 0 0 -1 0 }{PSTYLE "Maple Output" 0 11 1 {CSTYLE "" -1 -1 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 }3 3 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }{PSTYLE "" 11 12 1 {CSTYLE "" -1 -1 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 }1 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }{PSTYLE "Maple Plot" 0 13 1 {CSTYLE "" -1 -1 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 }3 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }{PSTYLE "Title" 0 18 1 {CSTYLE "" -1 -1 "" 1 18 0 0 0 0 0 1 1 0 0 0 0 0 0 }3 0 0 -1 12 12 0 0 0 0 0 0 19 0 }{PSTYLE " " 0 256 1 {CSTYLE "" -1 -1 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 }3 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }{PSTYLE "" 0 257 1 {CSTYLE "" -1 -1 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 }3 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }{PSTYLE "" 0 258 1 {CSTYLE "" -1 -1 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 }3 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }{PSTYLE "" 0 259 1 {CSTYLE "" -1 -1 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 }3 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }{PSTYLE "" 0 260 1 {CSTYLE "" -1 -1 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 }3 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }{PSTYLE "" 0 261 1 {CSTYLE "" -1 -1 "" 0 1 0 0 0 0 0 0 0 0 0 0 0 0 0 }3 0 0 -1 -1 -1 0 0 0 0 0 0 -1 0 }} {SECT 0 {EXCHG {PARA 18 "" 0 "" {TEXT -1 66 "Computer Problem 2: The u nicycle model of an automobile suspension" }}}{EXCHG {PARA 3 "" 0 "" {TEXT -1 12 "Introduction" }}}{EXCHG {PARA 0 "" 0 "" {TEXT -1 20 "Form ula (21), p.165 " }}{PARA 256 "" 0 "" {XPPEDIT 18 0 "G = F[0]/sqrt((k- m*omega^2)^2+(c*omega)^2);" "6#/%\"GG*&&%\"FG6#\"\"!\"\"\"-%%sqrtG6#,& *$,&%\"kGF**&%\"mGF**$%&omegaG\"\"#F*!\"\"\"\"#F**$*&%\"cGF*F5F*\"\"#F *F7" }{TEXT -1 0 "" }}{PARA 0 "" 0 "" {TEXT -1 96 "gives the amplitude of vibration of the steady-state solution to the damped mass-spring e quation" }}{PARA 257 "" 0 "" {XPPEDIT 18 0 "m*`@@`(D,2)(x)+c*D(x)+k*x \+ = F[0]*cos(omega*t);" "6#/,(*&%\"mG\"\"\"--%#@@G6$%\"DG\"\"#6#%\"xGF'F '*&%\"cGF'-F,6#F/F'F'*&%\"kGF'F/F'F'*&&%\"FG6#\"\"!F'-%$cosG6#*&%&omeg aGF'%\"tGF'F'" }{TEXT -1 0 "" }}{PARA 0 "" 0 "" {TEXT -1 38 "The first thing we want to do is plot " }{XPPEDIT 18 0 "G;" "6#%\"GG" }{TEXT -1 39 " vesrsus the driving angular frequency " }{XPPEDIT 18 0 "omega; " "6#%&omegaG" }{TEXT -1 0 "" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 8 "restart;" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 43 "Gx := F0/s qrt((k-m*omega^2)^2+(c*omega)^2);" }}{PARA 11 "" 1 "" {XPPMATH 20 "6#> %#GxG*&%#F0G\"\"\"*$-%%sqrtG6#,**$)%\"kG\"\"#F'\"\"\"*(F/F1%\"mGF1)%&o megaGF0F'!\"#*&)F3F0F')F5\"\"%F'F1*&)%\"cGF0F'F4F'F1F'!\"\"" }}} {EXCHG {PARA 0 "" 0 "" {TEXT -1 15 "We now use the " }{TEXT 257 7 "una pply" }{TEXT -1 17 " command to make " }{XPPEDIT 18 0 "G;" "6#%\"GG" } {TEXT -1 15 " a function of " }{XPPEDIT 18 0 "omega;" "6#%&omegaG" } {TEXT -1 1 " " }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 23 "G := unapp ly(Gx,omega);" }}{PARA 11 "" 1 "" {XPPMATH 20 "6#>%\"GGR6#%&omegaG6\"6 $%)operatorG%&arrowGF(*&%#F0G\"\"\"*$-%%sqrtG6#,**$)%\"kG\"\"#F.\"\"\" *(F6F8%\"mGF8)9$F7F.!\"#*&)F:F7F.)F<\"\"%F.F8*&)%\"cGF7F.F;F.F8F.!\"\" F(F(F(" }}}{EXCHG {PARA 0 "" 0 "" {TEXT -1 100 "Later we will want to \+ plot solutions to the mass-spring differential equation so let's enter it also" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 67 "diffeq := m*dif f(x(t),t$2)+c*diff(x(t),t)+k*x(t) = F0*cos(omega*t);" }}{PARA 11 "" 1 "" {XPPMATH 20 "6#>%'diffeqG/,(*&%\"mG\"\"\"-%%diffG6$-%\"xG6#%\"tG-% \"$G6$F0\"\"#F)F)*&%\"cGF)-F+6$F-F0F)F)*&%\"kGF)F-F)F)*&%#F0GF)-%$cosG 6#*&%&omegaGF)F0F)F)" }}}{EXCHG {PARA 0 "" 0 "" {TEXT -1 47 "Let us us e the parameters of Example 6, p. 166:" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 34 "m := 1; c := 2; k := 26; F0 := 82;" }}{PARA 11 "" 1 " " {XPPMATH 20 "6#>%\"mG\"\"\"" }}{PARA 11 "" 1 "" {XPPMATH 20 "6#>%\"c G\"\"#" }}{PARA 11 "" 1 "" {XPPMATH 20 "6#>%\"kG\"#E" }}{PARA 11 "" 1 "" {XPPMATH 20 "6#>%#F0G\"##)" }}}{EXCHG {PARA 0 "" 0 "" {TEXT -1 9 "P lotting " }{XPPEDIT 18 0 "G;" "6#%\"GG" }{TEXT -1 9 " against " } {XPPEDIT 18 0 "omega;" "6#%&omegaG" }{TEXT -1 27 " gives Figure 2.6.9, p. 167" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 27 "plot(G(omega),om ega=0..10);" }}{PARA 13 "" 1 "" {GLPLOT2D 399 225 225 {PLOTDATA 2 "6%- %'CURVESG6$7jn7$\"\"!$\"1ah%Q:YQ:$!#:7$$\"1nmm;arz@!#;$\"1l\\5uUbsJF+7$$\"1nmm\"z_\"4iF/$\"1K\\%[bgv>$F+7$$ \"1ommT&phN)F/$\"1#)RpHl$QB$F+7$$\"1LLe*=)H\\5F+$\"1;S&H#Gn\"G$F+7$$\" 1nm\"z/3uC\"F+$\"1)z69MtsL$F+7$$\"1++DJ$RDX\"F+$\"19ODy1G2MF+7$$\"1nm \"zR'ok;F+$\"1=!oz'pQ%\\$F+7$$\"1++D1J:w=F+$\"1)Q'4T>!zf$F+7$$\"1MLL3E n$4#F+$\"14Td5P;CPF+7$$\"1nm;/RE&G#F+$\"11Ljc0TaQF+7$$\"1+++D.&4]#F+$ \"1#GdLyOd-%F+7$$\"1+++vB_eWF+7$$\"1nm\"z*ev:JF+$\"1\"zqP^))4q%F+7$$\"1MLL347TLF+$\"1zx'eO_#R] F+7$$\"1MLLLY.KNF+$\"1Ouz%Q\"3u`F+7$$\"1++D\"o7Tv$F+$\"1SJ4>aSDeF+7$$ \"1LLL$Q*o]RF+$\"113=vuB\"G'F+7$$\"1,+D\"=lj;%F+$\"1$H*f1twIoF+7$$\"1+ +vV&R.)F+7$$\"1MLeR\"3Gy%F+$\"1`-Yc(>'[\")F+7$$\"1\\i:N,M4[ F+$\"15$yTqC\"p\")F+7$$\"1m\"H28se$[F+$\"13*HumpX=)F+7$$\"1$3-j7/C'[F+ $\"18I^<)yZ>)F+7$$\"1+](=7O*))[F+$\"1N`B@Qg*>)F+7$$\"1)F+7$$\"1M3-8,+U\\F+$\"1=y<06m#>)F+7$$\"1^Pf3@`o\\F+$\"1&* *GT+c2=)F+7$$\"1nm;/T1&*\\F+$\"1'**yJ$\\>j\")F+7$$\"1m;/^7I0^F+$\"1?j- i'42.)F+7$$\"1nm\"zRQb@&F+$\"1!*eC71Y4yF+7$$\"1MLLe,]6`F+$\"1X\\vWD+dv F+7$$\"1++v=>Y2aF+$\"18&F+7$$\"1,+D\"y%3TiF+$\"1$)[5(3<)eXF+7$$\"1++]P![hY'F+$\"1( *H:v*HW,%F+7$$\"1LLL$Qx$omF+$\"135')our*f$F+7$$\"1+++v.I%)oF+$\"1;KdzZ 5BKF+7$$\"1mm\"zpe*zqF+$\"1sH-\")zEJHF+7$$\"1,++D\\'QH(F+$\"1%\\MN[/nl #F+7$$\"1LLe9S8&\\(F+$\"1P_\"\\R'eLCF+7$$\"1,+D1#=bq(F+$\"17W&z631B#F+ 7$$\"1LLL3s?6zF+$\"1kh.n:5d?F+7$$\"1++DJXaE\")F+$\"1tUg,qa(*=F+7$$\"1o mmm*RRL)F+$\"1_#>9Dm=w\"F+7$$\"1om;a<.Y&)F+$\"17DlN%f&Q;F+7$$\"1NLe9tO c()F+$\"1#*>d#RG%H:F+7$$\"1,++]Qk\\*)F+$\"1z)eVG*3R9F+7$$\"1NL$3dg6<*F +$\"1?][$>ncM\"F+7$$\"1ommmxGp$*F+$\"1aJgwK3q7F+7$$\"1++D\"oK0e*F+$\"1 9$ztfEn>\"F+7$$\"1,+v=5s#y*F+$\"1&eY:UlE8\"F+7$$\"#5F($\"1w`3.qsp5F+-% 'COLOURG6&%$RGBG$Fe^l!\"\"F(F(-%+AXESLABELSG6$Q&omega6\"%!G-%%VIEWG6$; F(Fd^l%(DEFAULTG" 1 2 0 1 0 2 9 1 4 2 1.000000 45.000000 45.000000 0 } }}}{EXCHG {PARA 11 "" 1 "" {TEXT -1 0 "" }}}{EXCHG {PARA 0 "" 0 "" {TEXT -1 31 "The resonant angular frequency " }{XPPEDIT 18 0 "omega[1] ;" "6#&%&omegaG6#\"\"\"" }{TEXT -1 94 " for a damped mass-spring syst em is defined to be the value of the driving angular frequency " } {XPPEDIT 18 0 "omega;" "6#%&omegaG" }{TEXT -1 125 " which maximizes th e amplitude of the steady-state oscillations. We can see form the grap h above that it is somewhere around " }{XPPEDIT 18 0 "omega = 5;" "6#/ %&omegaG\"\"&" }{TEXT -1 30 ". To find it exactly we solve " } {XPPEDIT 18 0 "d*G/(d*omega) = 0;" "6#/*(%\"dG\"\"\"%\"GGF&*&F%F&%&ome gaGF&!\"\"\"\"!" }{TEXT -1 5 " for " }{XPPEDIT 18 0 "omega;" "6#%&omeg aG" }{TEXT -1 1 "." }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 36 "solve (diff(G(omega),omega)=0,omega);" }}{PARA 11 "" 1 "" {XPPMATH 20 "6%\" \"!,$*$-%%sqrtG6#\"\"'\"\"\"\"\"#,$F%!\"#" }}}{EXCHG {PARA 0 "" 0 "" {TEXT -1 42 "and thus the resonant angular frequency is" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 20 "omega1 := 2*sqrt(6);" }}{PARA 11 " " 1 "" {XPPMATH 20 "6#>%'omega1G,$*$-%%sqrtG6#\"\"'\"\"\"\"\"#" }}} {EXCHG {PARA 0 "" 0 "" {TEXT -1 137 "We now want to plot some solution s to the differential equations corresponding to different values of t he driving angular frequency, say " }{XPPEDIT 18 0 "omega = omega[1]; " "6#/%&omegaG&F$6#\"\"\"" }{TEXT -1 1 "," }{XPPEDIT 18 0 "omega[1]/2; " "6#*&&%&omegaG6#\"\"\"\"\"\"\"\"#!\"\"" }{TEXT -1 6 ", and " } {XPPEDIT 18 0 "2*omega[1];" "6#*&\"\"#\"\"\"&%&omegaG6#\"\"\"F%" } {TEXT -1 28 " whose numerical values are " }}}{EXCHG {PARA 0 "> " 0 " " {MPLTEXT 1 0 48 "evalf(omega1); evalf(omega1/2); evalf(2*omega1);" } }{PARA 11 "" 1 "" {XPPMATH 20 "6#$\"+'[z*)*[!\"*" }}{PARA 11 "" 1 "" {XPPMATH 20 "6#$\"+V(*[\\C!\"*" }}{PARA 11 "" 1 "" {XPPMATH 20 "6#$\"+ s*ezz*!\"*" }}}{EXCHG {PARA 0 "" 0 "" {TEXT -1 83 "The amplitude of th e steady-state oscillations at these three frequencies should be" }}} {EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 57 "evalf(G(omega1)); evalf(G(om ega1/2)); evalf(G(2*omega1));" }}{PARA 11 "" 1 "" {XPPMATH 20 "6#$\"++ +++#)!\"*" }}{PARA 11 "" 1 "" {XPPMATH 20 "6#$\"+N?F#)R!\"*" }}{PARA 11 "" 1 "" {XPPMATH 20 "6#$\"+X11G6!\"*" }}}{EXCHG {PARA 0 "" 0 "" {TEXT -1 137 "To verify that the predicted apmplitudes of the steady-s tate solution at these frequencies are correct we solve the differenti al equation" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 7 "diffeq;" }} {PARA 11 "" 1 "" {XPPMATH 20 "6#/,(-%%diffG6$-%\"xG6#%\"tG-%\"$G6$F+\" \"#\"\"\"-F&6$F(F+F/F(\"#E,$-%$cosG6#*&%&omegaGF0F+F0\"##)" }}}{EXCHG {PARA 0 "" 0 "" {TEXT -1 28 "with the initial conditions " }{XPPEDIT 18 0 "x(0) = 6;" "6#/-%\"xG6#\"\"!\"\"'" }{TEXT -1 2 ", " }{XPPEDIT 18 0 "D(x)(0) = 0;" "6#/--%\"DG6#%\"xG6#\"\"!F*" }{TEXT -1 15 " using \+ Maple's " }{TEXT 256 6 "dsolve" }{TEXT -1 8 " command" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 49 "xsoln1 := dsolve(\{diffeq,x(0)=6,D( x)(0)=0\},x(t));" }}{PARA 12 "" 1 "" {XPPMATH 20 "6#>%'xsoln1G/-%\"xG6 #%\"tG,(*&,Z*&-%$sinG6#,$F)\"\"&\"\"\"-F/6#*&,&!\"&F3%&omegaGF3F3F)F3F 3!$I\"*&-%$cosGF0F3-F=6#*&,&F2F3F9F3F3F)\"\"\"F3\"$I\"*&FFB)F9\"\"$F BF3*(FFBF9FB !#5*(FFBFLFBF8*(FFBF9FB!#C*(FFBFLFBF3*(F.FBFEFBFLFBF8*(F.FBFEFBF9 FBFZ*(F.FBFEFBFOFBF3*&F.FBFHFBFJ*&F.FBF>FBFJ*&F.FBFEFBFCFB,(*$)F9\"\"% FBF3*$FLFB!#[\"$w'F3!\"\"#\"#TF2*&*(,(Fio!$.\"\"$i*F3FfoFPF3-%$expG6#, $F)FRF3F " 0 "" {MPLTEXT 1 0 39 "xo := un apply(subs(xsoln1,x(t)),omega):" }}}{EXCHG {PARA 0 "" 0 "" {TEXT -1 90 "and plot the solution for the three values of the driving angular \+ frequncy indicated above" }}}{EXCHG {PARA 0 "> " 0 "" {MPLTEXT 1 0 75 "plot(\{xo(omega1),xo(omega1/2),xo(2*omega1)\},t=0..8,color=[red,blue, black]);" }}{PARA 13 "" 1 "" {GLPLOT2D 399 221 221 {PLOTDATA 2 "6'-%'C URVESG6$7iz7$\"\"!$\"\"'F(7$$\"1nmm;arz@!#<$\"1h*zV%Gn#)f!#:7$$\"1LLLL 3VfVF.$\"1[Ar9f5E$FD$\"1gs/m8kcFF 17$$\"1LL$e/&f(o$FD$\"1s4I%3yT&>F17$$\"1+++v2<9TFD$\"1EH!*)\\1d4\"F17$ $\"1nm;/luSXFD$\"1y\"*)>*o(o'>FD7$$\"1LLLLAKn\\FD$!1[9ixf%=C(FD7$$\"1L LL$eDnR&FD$!1p5.Z;]KcF17$$\"1mmmmY/$e*FD$!1r9,ZzY`_F17$$\"1LLL$Q k#z**FD$!1Y/[r'p)*p%F17$$\"1+++&p_*Q5F1$!1N\\F0lpaRF17$$\"1mmm^*y*z5F1 $!1es(*pf,aIF17$$\"1LLL3_+@6F1$!1r)4/zbV-#F17$$\"1+++l9.i6F1$!1$ze8.aX )*)FD7$$\"1LLLy3Y/7F1$\"1$HdBe(3oKFD7$$\"1mmm\"H!*oC\"F1$\"1n$o='R$*G\"F1$\"1cHGc\\\"ox#F17$$\"1LLL=\"\\CF17$$\"1LL LB6@G=F1$\"1w\\\"*e_Mw6F17$$\"1++]2%[8(=F1$!1;@a&R&ygGFD7$$\"1nmm\"p&[ 9>F1$!1D9xDMwaF1$!1%Q$=%)p&f;$F17$$\"1+++g-w+?F1$!1u KHOEQdWF17$$\"1+++qY2W?F1$!1BZ]v(4_d&F17$$\"1+++!3*Q(3#F1$!1&=J!e8FikF 17$$\"1+++!\\.28#F1$!1*[P$HDcwqF17$$\"1++++z,u@F1$!1\"=!G8:q(Q(F17$$\" 1+++I'))[>#F1$!1Z]rZkxBuF17$$\"1+++g$fd@#F1$!1$f%R#*Q\\%Q(F17$$\"1+++! 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Example 5, p.163)." }}{PARA 0 "" 0 "" {TEXT -1 44 " 1. a. The differential equation has the form" }}{PARA 259 "" 0 "" {TEXT -1 0 "" }{XPPEDIT 18 0 "m*`@@`(D,2)(x)+c*D(x)+k*x = E[0]*cos(ome ga*t)+F[0]*sin(omega*t);" "6#/,(*&%\"mG\"\"\"--%#@@G6$%\"DG\"\"#6#%\"x GF'F'*&%\"cGF'-F,6#F/F'F'*&%\"kGF'F/F'F',&*&&%\"EG6#\"\"!F'-%$cosG6#*& %&omegaGF'%\"tGF'F'F'*&&%\"FG6#F;F'-%$sinG6#*&F@F'FAF'F'F'" }{TEXT -1 0 "" }}{PARA 0 "" 0 "" {TEXT -1 63 "Recall that the general solution t o this equation has the form " }{XPPEDIT 18 0 "x = x[c]+x[p];" "6#/%\" xG,&&F$6#%\"cG\"\"\"&F$6#%\"pGF)" }{TEXT -1 7 " where " }{XPPEDIT 18 0 "x[c];" "6#&%\"xG6#%\"cG" }{TEXT -1 18 " is transient and " } {XPPEDIT 18 0 "x[p];" "6#&%\"xG6#%\"pG" }{TEXT -1 43 " is the steady-s tate part of the solution. " }{TEXT -1 0 "" }{TEXT -1 51 "The appropri ate guess for a particular solution is " }{XPPEDIT 18 0 "x[p] = A*cos( omega*t)+B*sin(omega*t);" "6#/&%\"xG6#%\"pG,&*&%\"AG\"\"\"-%$cosG6#*&% &omegaGF+%\"tGF+F+F+*&%\"BGF+-%$sinG6#*&F0F+F1F+F+F+" }{TEXT -1 60 ". \+ Substitute this into the differential equation, solve for " }{XPPEDIT 18 0 "A;" "6#%\"AG" }{TEXT -1 6 " and ," }{XPPEDIT 18 0 "B;" "6#%\"BG " }{TEXT -1 37 " and thereby show that the amplitude " }{XPPEDIT 18 0 "sqrt(A^2+B^2);" "6#-%%sqrtG6#,&*$%\"AG\"\"#\"\"\"*$%\"BG\"\"#F*" } {TEXT -1 1 " " }{TEXT -1 22 "of the steady-state is" }}{PARA 260 "" 0 "" {XPPEDIT 18 0 "G = sqrt(E[0]^2+F[0]^2)/sqrt((k-m*omega^2)^2+(c*omeg a)^2);" "6#/%\"GG*&-%%sqrtG6#,&*$&%\"EG6#\"\"!\"\"#\"\"\"*$&%\"FG6#F. \"\"#F0F0-F'6#,&*$,&%\"kGF0*&%\"mGF0*$%&omegaG\"\"#F0!\"\"\"\"#F0*$*&% \"cGF0F?F0\"\"#F0FA" }{TEXT -1 0 "" }{TEXT -1 1 "." }}{PARA 0 "" 0 "" {TEXT -1 86 "Show that for the unicycle model of an automobile suspens ion this leads to the formula" }}{PARA 261 "" 0 "" {XPPEDIT 18 0 "G = \+ a*sqrt(k^2+(2*c*Pi*v/L)^2)/sqrt((k-m*(2*Pi*v/L)^2)^2+(2*c*Pi*v/L)^2); " "6#/%\"GG*(%\"aG\"\"\"-%%sqrtG6#,&*$%\"kG\"\"#F'*$*,\"\"#F'%\"cGF'%# PiGF'%\"vGF'%\"LG!\"\"\"\"#F'F'-F)6#,&*$,&F-F'*&%\"mGF'*$**\"\"#F'F3F' F4F'F5F6\"\"#F'F6\"\"#F'*$*,\"\"#F'F2F'F3F'F4F'F5F6\"\"#F'F6" }{TEXT -1 0 "" }{TEXT -1 0 "" }{TEXT -1 0 "" }}{PARA 0 "" 0 "" {TEXT -1 66 "f or the amplitude of the steady-state vibrations versus the speed " } {XPPEDIT 18 0 "v;" "6#%\"vG" }{TEXT -1 10 " (in m/s) " }{TEXT -1 11 "o f the car." }}{PARA 0 "" 0 "" {TEXT -1 44 "b. Using the parameters giv en in Example 5: " }{XPPEDIT 18 0 "m = 800;" "6#/%\"mG\"$+)" }{TEXT -1 5 " kg, " }{XPPEDIT 18 0 "c = 3000;" "6#/%\"cG\"%+I" }{TEXT -1 8 " \+ N-s/m, " }{XPPEDIT 18 0 "k = 70000;" "6#/%\"kG\"&++(" }{TEXT -1 6 " N/ m, " }{XPPEDIT 18 0 "a = .5e-1;" "6#/%\"aG$\"\"&!\"#" }{TEXT -1 4 " m, " }{XPPEDIT 18 0 "L = 10;" "6#/%\"LG\"#5" }{TEXT -1 148 " m obtain th e graph of steady-state amplitude versus velocity given in Figure 2.6. 12, p. 169 (see p. 164 for the conversion factor from m/s to mph)." }} {PARA 0 "" 0 "" {TEXT -1 25 "c. The resonant velocity " }{XPPEDIT 18 0 "v[1];" "6#&%\"vG6#\"\"\"" }{TEXT -1 45 " is apparently about 30 mph . Find it exactly." }}{PARA 0 "" 0 "" {TEXT -1 49 "d. Use Maple's dsol ve command to plot the motion " }{XPPEDIT 18 0 "x(t);" "6#-%\"xG6#%\"t G" }{TEXT -1 42 " of a unicycle corresponding to speeds of " } {XPPEDIT 18 0 "v[1];" "6#&%\"vG6#\"\"\"" }{TEXT -1 2 ", " }{XPPEDIT 18 0 "v[1]/2;" "6#*&&%\"vG6#\"\"\"\"\"\"\"\"#!\"\"" }{TEXT -1 5 " and \+ " }{XPPEDIT 18 0 "2*v[1];" "6#*&\"\"#\"\"\"&%\"vG6#\"\"\"F%" }{TEXT -1 29 " assuming initial conditions " }{XPPEDIT 18 0 "x(0) = 0;" "6#/- %\"xG6#\"\"!F'" }{TEXT -1 2 ", " }{XPPEDIT 18 0 "D(x)(0) = 0;" "6#/--% \"DG6#%\"xG6#\"\"!F*" }{TEXT -1 1 "." }}{PARA 0 "" 0 "" {TEXT -1 0 "" }}{PARA 0 "" 0 "" {TEXT -1 38 "2. The value of the damping parameter \+ " }{XPPEDIT 18 0 "c;" "6#%\"cG" }{TEXT -1 50 " which would make the sy stem critically damped is " }{XPPEDIT 18 0 "c[cr] = 2*sqrt(m*k);" "6#/ &%\"cG6#%#crG*&\"\"#\"\"\"-%%sqrtG6#*&%\"mGF*%\"kGF*F*" }{TEXT -1 100 " which for the given mass and spring constant has a value of about 15 000 N-s/m. Thus for the value, " }{XPPEDIT 18 0 "c = 3000;" "6#/%\"cG \"%+I" }{TEXT -1 104 ", given above the suspension is (very) underdamp ed. Plot the steady-state amplitude versus velocity for " }{XPPEDIT 18 0 "c = 10000;" "6#/%\"cG\"&++\"" }{TEXT -1 17 " (underdamped), " } {XPPEDIT 18 0 "c = c[cr];" "6#/%\"cG&F$6#%#crG" }{TEXT -1 26 " (critic ally damped) and " }{XPPEDIT 18 0 "c = 30000;" "6#/%\"cG\"&++$" } {TEXT -1 124 " (overdamped). Discuss the advantages and disadvantages \+ of different amounts of damping in relation to the speed of the car." }}}}{MARK "29 1 0" 0 }{VIEWOPTS 1 1 0 1 1 1803 }