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Chapter 3 (maths 3)

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Chapter 3 (maths 3)

1. 1. CHAPTER 3APPLICATION OF PARTIAL DIFFERENTIAL EQUATIONS In many physical and engineering problems, we always seek a solution of thedifferential equations, whether it is ordinary or partial, which satisfies some specifiedconditions called the boundary conditions. Any differential equations together with these boundary conditions is calledboundary value problem. In this chapter we shall study some of the most important partial differentialequations occurring in engineering applications. One of the most fundamental common phenomena that are found in nature is thephenomena of wave motion. When a stone is dropped in to a pound, the surface of wateris disturbed and waves of displacement travel rapidly outward. When a bell or tuning forkis struck, sound waves are propagated from the source of sound. Whatever is the nature of wave phenomena, whether it is the displacement of atightly stretched string, the deflection of a stretched membrane, the propagation ofcurrents and potentials along an electrical transmission line, these entities are governedby a partial differential equation, known as the Wave Equation. ∂2 y 2 ∂ y 2Variable Separable Solution of the Wave Equation 2 = a ∂t ∂x 2Let y ( x, t ) = X ( x ).T ( t ) …..…… (1)be the solution of the equation ∂2 y 2 ∂ y 2 =a ….……. (2) ∂t 2 ∂x 2Where X ( x ) is a function of ‘ x ’alone and T ( t ) is a function of‘t’ alone.Then ∂2 y ∂2 y d 2T d 2x = XT ′′ and =X ′′T , Where T ′′ = 2 and X ′′ = 2 Satisfy equation (2) ∂t 2 ∂x 2 dt dxi.e., XT ′′ = a x ′′T 2 X ′′ T ′′ = 2  (3) X a TThe L.H.S of (3) is a function of x alone and the R.H.S is a function of t alone. They areequal for all values of the independent variable x and t. This is possible only if each is aconstant. X ′′ T ′′ = 2 =k , Where k is a constant. X a T 1
2. 2. X ′′ = kX = 0 ……….. (4)and T ′′ − ka 2T = 0 ……….. (5)The nature of the solution of (4) and (5) depends on the nature of values of k. Hence thefollowing three cases arise.Case 1: k is positive. Let k = p 2Then equation (4) and (5) become (D2 − p2 )X = 0and ( D′ 2 − p 2 a 2 )T = 0 d dWhere D≡ and D ′ ≡ dx dtThe solutions of these equations are X = Ae px + Be − pxand T = Ce pat + De − patCase 2:k is negative. Let k = − p 2Then equation (4) and (5) become (D2 + p2 )X = 0and ( D′ 2 + p 2 a 2 )T = 0The solutions of these equations are X = A cos px + B sin pxand T = C cos pat + D sin patCase 3:k = 0.Then equation (4) and (5) become d2X =0 dx 2 d 2Tand =0 dt 2The solutions of these equations are X = Ax + Band T = Ct + DSince y ( x, t ) = X .T is the solution of the wave equation, the three mathematicallypossible solutions of the wave equations are 2
3. 3. y ( x, t ) = ( Ae px + Be − px )( Ce pat + De − pat ) ……… (6) y ( x, t ) = ( A cos px + B sin px )( C cos pat + D sin pat ) ………. (7)and y ( x, t ) = ( Ax + B )( Ct + D ) ……… (8)Problems:(1)A uniform string is stretched and fastened to two points l apart. Motion is startedby displacing the string into the form of the curve 3  πx  (i) y = k sin   and  l  (ii) y = kx( l − x )and then releasing it from this position at time t=0. Find the displacement of thepoint of the string at a distance x from one end at time t.Solution: fig.1The displacement y ( x, t ) of the point of the string at a distance x from the left end 0 attime t is given by the equation (fig.1). ∂2 y ∂2 y = a2 2 ………… (1) ∂t 2 ∂xSince the ends of the string x=0 and x=l are fixed, they do not undergo any displacementat any time.Hence y ( x, t ) = 0, for t ≥ 0 ……. (2)and y ( l , t ) = 0, for t ≥ 0 ……. (3)Since the string is released from rest initially, that is , at t=0, the initial velocity of everypoint of the string in the y-direction is zero.Hence ∂y ( x,0) = 0, for 0 ≤ x ≤ l ……….. (4) ∂tSince the string is initially displaced in to the form of the curve y = f ( x ) , the coordinates{ x, y ( x,0)} satisfy the equation y = f ( x ) , where y ( x,0) is the initial displacement of thepoint ‘x’ in the y-direction. 3
4. 4. Hence y ( x,0) = f ( x ) , for 0 ≤ x ≤ l ………. (5)Where in (i) and in (ii). Conditions (2),(3),(4) and (5) are collectively called boundaryconditions of the problem. We have to get the solution of equation (1), the appropriatesolution, consistent with the vibration of the string is y ( x, t ) = ( A cos px + B sin px )( C cos pat + D sin pat ) ……… (6) Where A, B, C, D and p are arbitrary constants that are to be found out by using theboundary conditions.Using boundary conditions (2) in (6), we have A( C cos pat + D sin pat ) = 0 for all t ≥ 0 A=0Using boundary conditions (3) in (6), we have B sin pl ( C cos pat + D sin pat ) = 0 for all t ≥ 0 B sin pl = 0 Either B = 0 or sin pl = 0If B=0, the solution becomes y ( x, t ) = 0, which is meaningless.sin pl = 0 pl = nπ nπ p= l Where n = 0,1,2  ∞Differentiating both sides of (6) partially with respect to t, we have ∂y ( x, t ) = ( B sin px ). pa( − C sin pat + D cos pat ) ……… (7) ∂t nπWhere p= lUsing boundary conditions (4) in (7), we have B sin px. pa.D = 0 for 0 ≤ x ≤ lAs B ≠ 0 and p ≠ 0, we get D = 0Using these values of A, p, D in (6), the solution reduces to nπx nπat y ( x, t ) = BC sin cos , where n = 1,2,3 ∞ l lTaking BC=k, Eq.(1) has infinitely many solutions given below. πx πat y ( x, t ) = k sin cos l l 2nπx 2πat y ( x, t ) = k sin cos l l 3nπx 3πat y ( x, t ) = k sin cos , etc. l lSince Eq.(1) is linear, a linear combination of the R.H.S members of all the abovesolutions is the general solution of Eq.(1).Thus the most general solution of Eq.(1) is 4
5. 5. ∞ nπx nπat y ( x, t ) = ∑ ( c n k ) sin cos n =1 l lor ∞ nπx nπaty ( x, t ) = ∑ λ n sin cos ..……….. (8) n =1 l lWhere λ n is yet to be found out.Using boundary conditions (5) in (8), we have ∞ nπx∑ λn sin l = f ( x ), for 0 ≤ x ≤ l n =1 ………… (9)If we can express f(x) in a series comparable with the L.H.S. series of (9), we can get thevalues of λ n . 3 πx(i) f ( x ) = k sin l k πx 3πx  =  3 sin − sin  4 l l Using this form of f(x) in (9) and comparing like terms, we get 3k kλ1 = , λ3 = − , λ2 = 0 = λ4 =  4 4Using these values in (8), the required solution is 3k πx πat k 3πx 3πat y ( x, t ) = sin cos − sin cos 4 l l 4 l l(ii) y = kx( l − x )If we expand f(x) as Fourier half-range sine series in ( 0, l ) , that is in the form ∞ nπx ∑ bn sin l n =1it is comparable with the L.H.S series of (9). nπx l 2Thus λ n = bn = ∫ f ( x ) sin dx, by Euler ′s formula l 0 l nπx 1 ∫ (lx − x ) sin l dx 2k = 2 l 0 l   nπx   nπx   nπx    − cos   − sin   cos  ( lx − x ) 2k  2  l  − ( l − 2x) l  + ( − 2)  l  = l   nπ   n 2π 2   n 3π 3           l   l 2   l 3  0  = 4kl 2 nπ 3 3 { 1 − ( − 1) n } 5
6. 6. 0, if n is even  =  8kl 2  3 3 , if n is odd n πUsing this value of λ n in (8), the required solution is y ( x, t ) = 8kl 2 ∞ 1 ( 2n − 1)πx cos ( 2n − 1)πat π3 ∑ ( 2n − 1) n =1 3 sin l l ∂2 y ∂2 y(2) Solve the one dimensional wave equation = a 2 2 in − l ≤ x ≤ l , t ≥ 0, ∂t 2 ∂x ∂ygiven that y ( − l , t ) = 0, y ( l , t ) = 0, ( x,0) = 0 and y ( x,0 ) = ( l − x ). b ∂t lSolution: Shifting the origin to the point ( − l ,0 ) , we get x = X − l and y = Y , Where ( X , Y )are the coordinates of the point (x, y) with reference to the new system of coordinateaxes. The differential equation in the new system is ∂2 y ∂2 y = a2 2 0 ≤ X ≤ 2l , t ≥ 0, ……….. (1) ∂t 2 ∂xThe boundary conditions become Y ( 0, t ) = 0 ………… (2) Y ( 2l , t ) = 0 .…..…… (3) for all t ≥ 0. ∂Y ( X ,0) = 0 ………. (4) ∂t b  X, in 0 ≤ X ≤ land Y ( X ,0) =  l  ……….(5)  b ( 2l − X ) , in l ≤ X ≤ 2l l Since the last boundary condition in the old system is b  l (1 + x ) , in − l ≤ x ≤ 0  y ( x,0) =   b (1 − x ) , in 0 ≤ x ≤ l l The required solution of equation (1) is 8b ∞ 1 πx nπX nπat Y ( X , t ) = 2 ∑ 2 sin sin cos π n =1 n 2 2l 2l nπSince sin , When n is an even integer, the solution can be rewritten as 2 8b ∞ 1 πx nπX nπat Y ( X ,t) = 2 ∑ sin sin cos Where 0 ≤ X ≤ 2l , t ≥ 0. π n =1,3,5, n 2 2 2l 2lChanging over to the old system of coordinates, the solution becomes 6
7. 7. πx nπ ( x + l ) cos nπat ∞ 8b 1 y ( x, t ) = ∑ sin sin π2 n =1, 3, 5 n 2 2 2l 2l nπNow sin ( x + l ) = sin  nπ + nπx    2l  2 2l  nπ nπx nπ nπx = sin cos + cos sin 2 2l 2 2l nπ nπx = sin cos , Since n is odd. 2 2lThe required solution is 8b ∞ 1 nπ nπx nπat y ( x, t ) = 2 ∑ sin 2 cos cos π n =1,3,5, n 2 2 2l 2l 8b ∞ 1 nπx nπat y ( x, t ) = 2 ∑ cos cos π n =1,3,5, n 2 2l 2lWhere − l ≤ x ≤ l and t ≥ 0.(3) A tightly stretched strings with fixed end points x=0 and x=50 is initially at restin its equilibrium position. If it is said to vibrate by giving each point a velocity 3 πx(i) v = v 0 sin and 50 πx 2πx(ii) v = v 0 sin cos , 50 50Find the displacement of any point of the string at any subsequent time.Solution: The displacement y(x, t) of any point ‘x’ of the string at any time‘t’ is given by ∂2 y 2 ∂ y 2 =a ……….. (1) ∂t 2 ∂x 2We have to solve equation (1) satisfying the following boundary conditions. y ( 0, t ) = 0, for t ≥ 0 ………… (2) y ( 50, t ) = 0, for t ≥ 0 ..………..(3) y ( x,0) = 0, for 0 ≤ x ≤ 50 ………… (4)Since the string is in its equilibrium position initially and so the initial displacement ofevery point of the string is zero. ∂y ( x,0) = f ( x ) , for 0 ≤ x ≤ 50 ...………. (5) ∂t πxwhere f ( x ) = v 0 sin 3 For (i) and 50 πx 2πx f ( x ) = v 0 sin cos , For (ii) 50 50The suitable solution of Eq (1), consistent with the vibration of the string, is 7
8. 8. y ( x, t ) = ( A cos px + B sin px )( C cos pat + D sin pat ) ..…….……(6)Using boundary conditions (2) in (6), we have A( C cos pat + D sin pat ) = 0 for all t ≥ 0 A=0Using boundary conditions (3) in (6), we have B sin 50 p ( C cos pat + D sin pat ) = 0 for all t ≥ 0 Either B = 0 or sin 50 p = 0If we assume that B=0, we get a trivial solution. sin 50 p = 0 50 p = nπ nπ p= 50 Where n = 0,1,2  ∞Using boundary conditions (4) in (6), we have B sin px.C = 0 for 0 ≤ x ≤ 50 As B ≠ 0, we get C = 0Using these values of A, p, C in (6), the solution reduces to nπx nπat y ( x, t ) = k sin sin , ...............(7) 50 50where k = BD and n = 1,2,3 ∞The most general solution of Eq.(1) is ∞ nπ nπat y ( x, t ) = ∑ λ n sin cos ...………. n =1 50 50(8)Differentiating both sides of (8) partially with respect to t, we have ∂y ( x, t ) = ∑  nπa .λn  sin nπx cos nπat ∞   . ....………. (9) ∂t n =1  50  50 50Using boundary condition (5) in (9), we have ∞  nπa  nπx ∂y ∑  50 λn  sin 50 = v. Since v = ∂t ( x,0) , n =1   πx(i) v = v 0 sin 3 and 50 v  πx 3πx  = 0  3 sin − sin  4 50 50  ∞  nπa  nπx v  πx 3πx  ∑  50 λn  sin 50 = 40  3 sin 50 − sin 50 . n =1    Comparing like terms, we get πa 3v 3πa v nπa λ1 = 0 , λ3 = − 0 and λ n = 0, for n = 2,4,5,6 ∞ 50 4 50 4 50 8
9. 9. 75v0 25v0 λ1 = , λ3 = − and λ2 = 0 = λ4 = λ5 =  2πa 6πaUsing these values in (8), the required solution is 75v0 πx πx 25v0 3πx 3πat y ( x, t ) = sin sin − sin sin 2πa 50 50 6πa 50 50 πx 2πx(ii) v = v0 sin cos 50 50 v  3πx πx  = 0  sin − sin  2 50 50  ∞  nπa  nπx v  3πx πx  ∑  50 λn  sin 50 = 20  sin 50 − sin 50 . n =1    Comparing like terms, we get πa v 3πa v nπa λ1 = − 0 , λ3 = 0 and λn = 0, for n = 2,4,5,6  ∞ 50 4 50 4 50 25v 0 25v 0 λ1 = − , λ3 = and λ 2 = 0 = λ4 = λ5 =  πa 3πaUsing these values in (8), the required solution is 25v 0 πx πat 25v0 3πx 3πat y ( x, t ) = − sin sin + sin sin πa 50 50 3πa 50 50(4) A taut string of length 2l , fastened at both ends, is disturbed from its position ofequilibrium by imparting to each of its points an initial velocity of magnitudek ( 2lx − x 2 ). Find the displacement function y ( x, t ) .Solution: The displacement y(x, t) of any point ‘x’ of the string at any time ‘t’ is given by ∂2 y 2 ∂ y 2 =a ……….. (1) ∂t 2 ∂x 2We have to solve equation (1) satisfying the following boundary conditions. y ( 0, t ) = 0, for t ≥ 0 ………… (2) y ( 2l , t ) = 0, for t ≥ 0 .……….. (3) y ( x,0) = 0, for 0 ≤ x ≤ 2l ...……… (4) ∂y ( x,0) = k ( 2lx − x 2 ), for 0 ≤ x ≤ 2l ………… (5) ∂tThe suitable solution of Eq (1), consistent with the vibration of the string, is y ( x, t ) = ( A cos px + B sin px )( C cos pat + D sin pat ) ………… (6)Using boundary conditions (2) in (6), we have A( C cos pat + D sin pat ) = 0 for all t ≥ 0 A=0Using boundary conditions (3) in (6), we have B sin 2lp ( C cos pat + D sin pat ) = 0 for all t ≥ 0 Either B = 0 or sin 2lp = 0 9
10. 10. If we assume that B=0, we get a trivial solution. sin 2lp = 0 2lp = nπ nπ p= 2l Where n = 0,1,2  ∞Using boundary conditions (4) in (6), we have B sin px.C = 0 for 0 ≤ x ≤ 2l As B ≠ 0, we get C = 0Using these values of A, p, C in (6), the solution reduces to nπx nπat y ( x, t ) = k sin sin , .............(7) 2l 2lwhere n = 0,1,2,3 ∞The most general solution of Eq.(1) is ∞ nπ nπat y ( x, t ) = ∑ λ n sin cos ………. (8) n =1 2l 2lDifferentiating both sides of (8) partially with respect to t, we have ∂y ( x, t ) = ∑  nπa .λn  sin nπx cos nπat ∞   ………. (9) ∂t n =1  2l  2l 2lUsing boundary condition (5) in (9), we have  nπa  nπx ∑  2l λn  sin 2l = k ( 2lx − x 2 ), for 0 ≤ x ≤ 2l ∞ n =1   ∞ nπx = ∑ bn sin n =1 2lWhich is Fourier half-range sine series of k ( 2lx − x 2 ). in ( 0,2l ) .Comparing like terms, we getnπa nπx 2l 2 .λ n = bn = ∫ f ( x ) sin dx, by Euler ′s formula 2l 2l 0 l nπx 2l = ∫ k ( 2lx − x 2 ) sin 2 dx 2l 0 2l 2l   nπx   nπx   nπx    − cos   − sin   cos  ( 2lx − x ) 2k  2  2l  − ( 2l − 2 x )  2l  + ( − 2)  2l  = nπa   nπ   n 2π 2   n 3π 3           2l   4l 2   8l 3  0  { } 3 32kl = 4 4 1 − ( − 1) n nπ a 10
11. 11. 0, if n is even  =  32kl 3  4 4 , if n is odd n π aUsing this value of λ n in (8), the required solution is y ( x, t ) = 64kl 3 ∞ 1 ( 2n − 1)πx cos ( 2n − 1)πat π 4a ∑ ( 2n − 1) n =1 4 sin 2l 2l ONE DIMENSIONAL HEAT FLOWVARIABLE SEPARABLE SOLUTIONS OF THE HEAT EQUATION The one dimensional heat flow equation is ∂u 2 ∂ u 2 =α .….……………..(1) ∂t ∂x 2Let u(x ,t) = X(x).T(t) …..……………..(2)be a solution of Eq.(1), where X(x) is a function of x alone and T(t) is a function of t ∂u ∂ 2u dT d2Xalone. Then = XT ′ and 2 = X ′′T , where T ′ = and X ′′ = , satisfy Eq. ∂t ∂x dt dx 2(1).i.e., XT ′ = α 2 X ′′T X ′′ T′i.e., = 2 ……..…………..(3) X α TThe L.H.S. of (3) is a function of x alone and the R.H.S is a function of t alone. They are equal for all values of independent variables x and t. This is possible onlyif each is a constant. X ′′ T′∴ = 2 = k, where k is a constant. X α T∴ X ′′ − kX = 0and T ′ − kα 2T = 0 …...……………(4)The nature of the solutions of (4) and (5) depends on the nature of the values of k. Hencethe following three cases come into being.Case 1 : k is positive. Let k = p 2 . Then equations (4) and (5) become ( D 2 − p 2 ) X = 0 and ( D′ − p 2α 2 )T = 0, where d d D≡ and D′ ≡ . dx dtThe solutions of these equations are 2 2 X = C1e px + C 2 e − px and T = C3e p α tCase 2 : k is negative. Let k = − p 2 . Then equations (4) and (5) become ( D 2 + p 2 ) X = 0 and ( D′ + p 2α 2 )T = 0,The solutions of these equations are 11
12. 12. 2 2 X = C1 cos px + C 2 sin px and T = C3 e − p α tCase 3 : k=0 Then equations (4) and (5) become d2X dT = 0 and =0 dx 2 dtThe solutions of these equations are X = C1 x + C 2 and T = C3Since u(x , t) = X.T is the solution of Eq.(1), the three mathematically possible solutionsof Eq.(1) are 2 2 u ( x , t ) = ( Ae px + Be − px )e p α t .…..…………….(6) 2 2 u ( x , t ) = ( A cos px + B sin px)e − p α t …..….…………(7)and u ( x , t ) = Ax + B …...……………(8)where C1C3 and C 2 C3 have been taken as A and B.PROBLEMS1. Find the temperature distribution in a homogeneous bar of length π which isinsulated laterally, if the ends are kept at zero temperature and if, initially, thetemperature is k at the centre of the bar and falls uniformly to zero at its ends.Solution: Figure 4.3 represents the graph of the initial temperature in the bar. y − 0 x −π 2k =Equation of OA is y = x and the equation of AB is k − 0 π π −π 2 2ki.e., y= (π − x) π 12
13. 13.  2k π  π x, in 0 ≤ x ≤  2Hence u ( x ,0) =   2k (π − x), in π ≤ x ≤ π π  2The temperature distribution u(x , t) in the bar is given by ∂u 2 ∂ u 2 =α ….……………..(1) ∂t ∂t 2We have to solve Eq.(1) satisfying the following boundary conditions. u (0 , t ) = 0, for all t ≥ 0 .….…………….(2) u (π , t ) = 0, for all t ≥ 0 ..….……………(3)  2k π  π x, in 0 ≤ x ≤  2 u ( x ,0) =  .…..……………(4)  2k (π − x), in π ≤ x ≤ π π  2As u(x , t) has to remain finite when t → ∞ , the proper solution of Eq.(1) is 2 2 u ( x , t ) = ( A cos px + B sin px)e − p α t …....….……….(5)Using boundary condition (2) in (5), we have 2 2 A.e − p α t = 0, for all t ≥ 0 ∴ A=0Using boundary condition (3) in (5), we have 2 2 B sin pπ .e − p α t = 0, for all t ≥ 0 ∴ B = 0 or sin pπ = 0 B = 0 leads to a trivial solution. sin pπ = 0 pπ = nπ or p = n, where n = 0 , 1 , 2,∞Using these values of A and p in (5), it reduces to 2 2 u ( x , t ) = B sin nx e − n α t ……………….(6)where n = 1 , 2 , 3, ∞ Therefore the most general solution of Eq.(1) is ∞ u ( x , t ) = ∑ Bn sin nx.e −n α 2 2 t ……………….(7) n =1Using boundary condition (4) in (7), we have ∞ ∑B n =1 n sin nx = f ( x) in (0, π ), where  2k π  π x, in 0 ≤ x ≤  2 f ( x) =   2k (π − x ), in π ≤ x ≤ π π  2 13
14. 14. ∞If the Fourier half-range sine series of f ( x) in (0, π ) is ∑ Bn sin nx, it is comparable with n =1 ∞∑Bn =1 n sin nx. π π  2  2 2k 2k  Hence Bn = bn =  ∫ x sin nx dx + ∫ (π − x) sin nx dx  π 0 π π π   2    π π  4k   − cos nx   − sin nx  2   − cos nx   − sin nx   = 2  x −  + (π − x) +  π   n   n 2  0   n   n 2  π    2 8k nπ = 2 2 sin nπ 2Using this value in (7), the required solution is 8k ∞ 1 nπ u ( x , t ) = 2 ∑ 2 sin 2 2 sin nx.e −n α t π n =1 n 2 8k ∞ (−1) n +1 ∑ (2n − 1) 2 sin(2n − 1) x.e −( 2n−1) α t 2 2 u( x , t) = π2 n =12. Solve the one dimensional heat flow equation ∂u ∂ 2u =α2 2 ∂t ∂xsatisfying the following boundary conditions. ∂u(i) (0 , t ) = 0, for all t ≥ 0 ∂x ∂u(ii) (π , t ) = 0, for all t ≥ 0; and ∂x(iii) u ( x ,0) = cos 2 x, 0 < x < πSolution: The appropriate solution of the equation ∂u ∂ 2u =α2 2 …………………(1) ∂t ∂xsatisfying the condition that u ≠ ∞ when t → ∞ is 2 2 u ( x , t ) = ( A cos px + B sin px)e − p α t ……..….……….(2)Differentiating (2) partially w.r.t. x, we have ∂u 2 2 ( x , t ) = p (− A sin px + B cos px )e − p α t ……..….………. ∂x(3)Using boundary condition (i) in (3), we have 14
15. 15. 2 2 p.B.e − p α t = 0, for all t ≥ 0∴ B=0 [ if p = 0, u ( x , t ) = A, which is meaningless ]Using boundary condition (ii) in (3), we have 2 2 − p. A sin pπ .e − p α t = 0, for all t ≥ 0∴ Either A = 0 or sin pπ = 0A = 0 leads to a trivial solution. sin pπ = 0 pπ = nπ or p = n, where n = 0 , 1 , 2,∞Using these values of B and p in (2), it reduces to 2 2 u ( x , t ) = A cos nx.e − n α t ………………..(4)where n = 0 , 1 , 2 , ∞ Therefore the most general solution of Eq.(1) is ∞ u ( x , t ) = ∑ An cos nx.e −n α 2 2 t .……………….(5) n=0Using boundary condition (iii) in (5), we have ∞ ∑A n =0 n cos nx = cos 2 x in (0, π )In general, we have to expand the function in the R.H.S. as a Fourier half-range cosineseries in (0, π ) so that it may be compared with L.H.S. series. 1 In this problem, it is not necessary. We can rewrite cos x as (1 + cos 2 x ), so that 2 2comparison is possible. ∞ 1 1Thus ∑ An cos nx = 2 + 2 cos 2 x n=0 Comparing like terms, we have 1 1 A0 = , A2 = , A1 = A3 = A4 =  = 0 2 2Using these values in (5), the required solution is 1 1 2 u ( x , t ) = + cos 2 x e −4α t 2 2 ∂u 2 ∂ u 23. Solve the equation =α satisfying the following conditions. ∂t ∂x 2(i) u is finite when t → ∞ . ∂u(ii) = 0 when x = 0, for all values of t. ∂x(iii) u = 0 when x = l, for all values of t.(iv) u = u 0 when t = 0, for 0 < x < l.Solution: We have to solve the equation 15
16. 16. ∂u ∂ 2u =α2 2 …………………(1) ∂t ∂xsatisfying the following boundary conditions. ∂u (0, t ) = 0, for all t ≥ 0 …………………(2) ∂x u(l , t) = 0, for all t ≥ 0 ………………....(3) u ( x , 0) = u 0 for 0 < x < l. ...………………(4)Since u is finite when t → ∞ , the proper solution of Eq.(1) is 2 2 u ( x , t ) = ( A cos px + B sin px)e − p α t ...…..….……….(5)Differentiating (5) partially w.r.t. x, we have ∂u 2 2 ( x , t ) = p (− A sin px + B cos px )e − p α t ……..….………. ∂x(6)Using boundary condition (ii) in (6), we have 2 2 p.B.e − p α t = 0, for all t ≥ 0∴ B=0 [ if p = 0, u ( x, t ) = A, which is meaningless ]Using boundary condition (iii) in (5), we have 2 2 − A cos pl.e − p α t = 0, for all t ≥ 0∴ Either A = 0 or cos pl = 0A = 0 leads to a trivial solution. cos pl = 0 π π pl = an odd multiple of or (2n − 1) 2 2 (2n − 1)π pl = , where n = 0 , 1 , 2,∞. 2lUsing these values of B and p in (5), it reduces to ( 2n − 1)πx −( 2 n −1)2 π 2α 2t 4l 2 u ( x , t ) = A cos . .e ….….…………..(7) 2lwhere n = 1 , 2 , 3 ,∞. Therefore the most general solution of Eq.(1) is ∞ (2n − 1)πx −( 2 n −1) 2 π 2t 4l 2 u ( x , t ) = ∑ A2 n−1 cos . .e ….….…………..(8) n =1 2lUsing boundary condition (iv) in (8), we have ∞ ( 2n − 1)πx ∑ A2n−1 cos . 2l = u0 in (0, l ) n =1 ………………….(9) 16
17. 17. The series in the L.H.S of (9) is not in the form of the Fourier half-range cosine series of a0 ∞ nπxany function in (0 , l), that is, + ∑ a n cos . Hence, to find A2 n−1, we proceed as in 2 n =1 lthe derivation of Euler’s formula for the Fourier coefficients. (2n − 1)πx Multiplying both sides of (9) by cos and integrating w.r.t. x between 0 2land l, we get 2 ( 2n − 1)πx (2n − 1)πx l l A2 n −1 ∫ cos dx = u 0 ∫ cos dx 0 2l 0 2l [ All other int egrals in the L.H .S . vanish] l l  (2n − 1)πx   (2n − 1)πx   sin   sin  1 l 2l A2 n −1 .  x +  = u0   2 (2n − 1)π   (2n − 1)π    l 0    2l 0  1 2l (2n − 1)π A2 n −1 . = u 0 . sin 2 (2n − 1)π 2 4u 0 A2 n −1 = ( −1) n +1 ( 2n − 1)πUsing this value in (8), the required solution is 4u o ∞ (−1) n +1 (2n − 1)πx ∑ (2n − 1) cos . 2l .e −( 2n−1) π α t 4l 2 2 2 2 u ( x, t ) = π n =1PROBLEMS ON TEMPERATURE IN A SLAB WITH FACES WITH ZEROTEMPERATURE1. Faces of a slab of width c are kept at temperature zero. If the initial temperaturein the slab is f (x) , determine the temperature formula. If f ( x) = u 0 , a constant, ∂ufind the flux − k ( x0 , t ) across any plane x = x0 (0 ≤ x0 ≤ c) and show that no heat ∂x cflows across the central plane x0 = , where k 2 is the diffusivity of the substance. 2Solution: 17
18. 18. Fig.3Though the slab is a three dimensional solid (Fig.2), it is assumed that the temperature init at a given time t depends only on and varies with respect to x, the distance measuredfrom one face along the width of the slab. Hence the temperature function u(x , t) at anyinterior point of the slab is given by ∂u ∂ 2u = k2 2 …………………(1) ∂t ∂xWe have to solve Eq.(1) satisfying the following boundary conditions. u(0 , t) = 0, for all t ≥ 0 ………………....(2) u(c , t) = 0, for all t ≥ 0 …………………(3) u(x , 0) = f (x) for 0 < x < c ………………....(4)Proceeding as before, the most general solution of Eq.(1) is ∞ nπx −n 2π 2k 2t c 2 u ( x , t ) = ∑ Bn sin . .e ….….…………..(5) n =1 cUsing boundary condition (4) in (5), we have ∞ nπx nπx ∑ Bn sin . c = f ( x) in (0, c) = ∑ bn sin c n =1which is the Fourier half-range sine series of f (x) in (0 , c).Comparing like terms, we get nπx c 2 Bn = bn = ∫ f ( x ) sin dx ………………… c0 c(6)Using (6) in (5), the required solution is nπx −n 2π 2k 2t c 2 nπθ c 2 ∞ u ( x , t ) = ∑ sin. .e ∫ f (θ ) sin c dθ …………………(7) c n =1 c 0When f ( x) = u 0 , from (6), we get 18
19. 19. nπx c 2 Bn = ∫ u 0 sin dx c0 c c  nπx  2u 0   cos = − c  c  nπ     c 0 2u = 0 {1 − cos nπ } c  4u 0  , if n is odd =  nπ 0,  if n is evenTherefore the required solution in this case is 4u 0 ∞ 1 (2n − 1)πx ∑ 2n − 1 sin. c .e −( 2n−1) π k t 2 2 2 c2 u( x , t) = …………………(8) c n=1Differentiating (8) partially w.r.t x, ∂u 4u ∞ (2n − 1)πx −( 2 n−1) 2 π 2 k 2t ∂x (x ,t) = 0 c ∑ cos. n =1 c .e c2Therefore the flux across the plane x = x0 is given by ∂u 4ku 0 ∞ (2n − 1)πx ∑ cos. c 0 .e −( 2n−1) π k t c 2 2 2 2 − k ( x0 , t ) = − ∂x c n =1 cTherefore the flux across the central plane x = is given by 2 ∂u  c  4ku 0 ∞ (2n − 1)π −( 2 n −1) 2 π 2 k 2t −k  ,t  = − ∂x  2  c n =1 ∑ cos.2 .e c2 (2n − 1)π = 0, sin ce cos =0 2That is no heat flow across the central plane of the slab.PROBLEMS WITH NON-ZERO BOUNDARY VALUES (TEMPERATURE ORTEMPERATURE GRADIENTS) 1. A bar AB with insulated sides is initially at temperature 0 0 C throughout. ∂u Heat is suddenly applied at the end x = l at a constant rate A, so that =A ∂x for x = l, while the end A is not disturbed. Find the subsequent temperature distribution in the bar. 19
20. 20. Solution: The temperature distribution u(x , t) in the bar is given by the equation. ∂u ∂ 2u =α2 2 …………………(1) ∂t ∂xWe have to solve Eq.(1) satisfying the following boundary conditions. u(0 , t) = 0, for all t ≥ 0 ………………....(3) ∂u (l , t ) = A, for all t ≥ 0 …………………(2) ∂x u ( x , 0) = 0 for 0 < x < l. ...……………….(4)Since condition (3) has a non-zero value on the right side, we adopt the modifiedprocedure.Let u ( x , t ) = u1 ( x) + u 2 ( x , t ) ………………….(5)Where u1 ( x) is given by d 2 u1 =0 .………………… dx 2(6)and u 2 ( x , t ) is given by ∂u 2 ∂ 2u2 =α2 .…………………(7) ∂t ∂x 2The boundary conditions for Eq.(6) are u1 (0) = 0 ………………….(8) du1and (l ) = A …………………(9) dxSolving Eq.(6), we get u1 ( x) = C1 x + C 2 ………………...(10)Using boundary condition (8) in (10), we get C 2 = 0From (10), we have du1 ( x) = C1 ..………………(11) dxUsing boundary condition (9) in (11), we get C1 = A. u1 ( x) = Ax ………………...(12)The boundary conditions for Eq.(7) are u 2 (0 , t ) = u (0 , t ) − u1 (0) = 0, for all t ≥ 0 ………………...(13) ∂u 2 ∂u du (l , t ) = (l , t ) − 1 (l ) = 0, for all t ≥ 0 ………………...(14) ∂x ∂x dx u 2 ( x ,0) = u ( x ,0) − u1 ( x ) = − Ax, for 0 < x < l ………………...(15) 20
21. 21. Proceeding as before, we get the most general solution of Eq.(7) as ∞ (2n − 1)πx  − (2n − 1) 2 π 2α 2 t  u 2 ( x , t ) = ∑ B2 n −1 sin exp  ………………...(16) n =1 2l  4l 2 Using boundary condition (15) in (16), we have ∞ (2n − 1)πx ∑B n =1 2 n −1 sin 2l = − Ax in (0 , l ) ( 2n − 1)πx l 2 ∴ B2 n−1 = ∫ − Ax sin 2l dx l 0 l   (2n − 1)πx   (2n − 1)πx    − cos 2A     − sin    x 2l 2l =−  −  l   (2n − 1)π   (2n − 1) π2 2      2l     4l 2  0  8 Al (2n − 1)π =− sin (2n − 1) π 2 2 2 8 Al.(−1) n = (2n − 1) 2 π 2Using this value in (16) and then using (12) and (16) in (5), the required solution is ∞ (2n − 1)πx  − (2n − 1) 2 π 2α 2 t  u ( x , t ) = ∑ B2 n−1 sin exp  n =1 2l  4l 2 Steady State Heat Flow in Two Dimensions:Variable Separable Solutions of Laplace Equation:Laplace equation in two dimensional Cartesians is ∂ 2u ∂ 2u + =0 …… (1) ∂x 2 ∂y 2Let u ( x, y ) = X ( x ).Y ( y ) …… (2)be the solution of the equation (1).Where X ( x ) is a function of ‘ x ’alone and Y ( y ) is a function of ‘y’ alone.Then ∂ 2u ∂ 2u d2X d2X = X ′′Y and 2 = XY ′′, Where X ′′ = and Y ′′ = Satisfy equation (1) ∂x 2 ∂y dx 2 dy 2 21
22. 22. X ′′Y + XY ′′ = 0 i.e X ′′ Y ′′ =−  (3) X YThe L.H.S of (3) is a function of x alone and the R.H.S is a function of t alone. They areequal for all values of the independent variable x and t. This is possible only if each is aconstant. X ′′ Y ′′ =− =k X YWhere k is a constant. X ′′ − kX = 0 …….. (4)and Y ′′ + kY = 0 …….. (5)The nature of the solution of (4) and (5) depends on the nature of values of k. Hence thefollowing three cases arise.Case 1: k is positive. Let k = p 2Then equation (4) and (5) become (D2 − p2 )X = 0and ( D′ 2 + p 2 )Y = 0Where d d D≡ and D ′ ≡ dx dYThe solutions of these equations are X = Ae px + Be − pxand Y = C cos py + D sin pyCase 2:k is negative. Let k = − p 2Then equation (4) and (5) become (D2 + p2 )X = 0and ( D′ 2 − p 2 )Y = 0The solutions of these equations are X = A cos px + B sin pxand Y = Ce py + De − pyCase 3:k = 0.Then equation (4) and (5) become 22
23. 23. d2X =0 dx 2and d 2Y =0 dy 2The solutions of these equations are X = Ax + Band Y = Cy + DSince u ( x, t ) = X ( x ).Y ( y ) is the solution of the equation (1), the three mathematicallypossible solutions of the equation (1) are u ( x, y ) = ( Ae px + Be − px )( C cos py + D sin py ) ……… (6) u ( x, y ) = ( A cos px + B sin px ) ( Ce + De ) py − py ………. (7)and u ( x, y ) = ( Ax + B )( Cy + D ) ……… (8)Problems:(1)A rectangular plane with insulated surface is a cm wide and so long compared toits width that it may be considered infinite in length without introducing anappreciable error. If the two long edges x=0 and x=a and the short edge at infinityare kept at temperature 0 0 C, while the other short edge y=0 is kept at temperature 3 πx(i) u 0 sin and (ii) T (constant). Find the steady state temperature at any point a(x, y) of the plate.Solution: . Fig.1 23
24. 24. The temperature u ( x, y ) at any point (x,y) of the plate in the steady state is given by theequation.. ∂ 2u ∂ 2u + =0 ………… (1) ∂x 2 ∂y 2We have to solve equation (1) satisfying the following boundary conditions. u ( 0, y ) = 0, for y>0 ……… (2) u ( a, y ) = 0, for y>0 ……….. (3) u ( x, ∞ ) = 0, for 0≤x≤a ……… (4) u ( x,0 ) = f ( x ) , for 0 ≤ x ≤ 2l ……… (5) πxWhere f ( x ) = u 0 sin for ( i ) and f ( x ) = T for ( ii ) 3 aThree possible solutions of the equation (1) are u ( x, y ) = ( Ae px + Be − px )( C cos py + D sin py ) ……… (6) u ( x, y ) = ( A cos px + B sin px ) ( Ce py + De − py ) ………. (7)and u ( x, y ) = ( Ax + B )( Cy + D ) ……… (8)By boundary condition (4), u → 0 when y → ∞. of the three possible solutions, onlysolution (7) can satisfy this condition. Hens we reject the other two solutions.Rewriting (7), we have u ( x, y ) e = py = ( A cos px + B sin px ) ( C + De −2 py ) ………. (9)Using boundary condition (4) in (9), we have ( A cos px + B sin px ) C = 0, for 0 ≤ x ≤ a C=0Using boundary conditions (2) in (7), we have A.D.e = py = 0 for all y > 0 Either A = 0 or D = 0If we assume that D=0, we get a trivial solution A=0Using boundary conditions (3) in (7), we have B sin pa.De = py = 0 for all y > 0The assumption that B=o leads to a trivial solution. 24
25. 25. sin pa = 0 pa = nπ nπ p= a Where n = 0,1,2  ∞Using these values of A, p, C in (7), the solution reduces to nπx − nπy a u ( x, y ) = λ sin e , ...........(10) awhere n = 0,1,2,3 ∞The most general solution of Eq.(1) is ∞ nπx −nπy a u ( x, y ) = ∑ λn sin e ………. (11) n =1 aUsing boundary conditions (5) in (11), we have ∞ nπx ∑ λn sin a = f ( x ) in ( 0, a ) n =1 ……… (12) πx(i) f ( x ) = u 0 sin 3 a u  πx 3πx  = 0  3 sin − sin  4 a a Using this form of f(x) in (12) and comparing like terms, we get 3u u λ1 = 0 , λ3 = − 0 , and λ 2 = 0 = λ 4 =  4 4Using these values in (11), the required solution is 3u πx −πy u 3πx −3πy a u ( x, y ) = 0 sin e a − 0 sin e 4 a 4 a(ii) f ( x ) = T in ( 0, a ) ∞ nπxLet the Fourier half-range sine series of f(x) in (o, a) be ∑b n =1 n sin aUsing this form of f(x) in (12) and comparing like terms, we get nπx a 2 λ n = bn = ∫ T sin dx a0 a a  nπx  − cos 2T    a  =   a  nπ    a   0 = 2T nπ { 1 − ( − 1) } n 25
26. 26. 0, if n is even  =  4T  nπ , if n is odd Using this value of λ n in (11), the required solution is u ( x, y ) = 4T π ∞ 1 ∑ ( 2n − 1) sin n =1 a { ( 2n − 1)πx exp − ( 2n − 1) πy a }(2) An infinitely long metal plate in the form of an area is enclosed between the lines y = 0 and y = π for positive values of x. The temperature is zero along the edges y = 0 , y = π and the edge at infinity. If the edge x=0 is kept at temperature ky, Find the steady state temperature distribution in the plate.Solution: Fig.2The temperature u ( x, y ) at any point (x, y) of the plate in the steady state is given by theequation.. ∂ 2u ∂ 2u + =0 ………… (1) ∂x 2 ∂y 2We have to solve equation (1) satisfying the following boundary conditions. u ( x,0 ) = 0, for x > 0 ……… (2) u ( x, π ) = 0, for x > 0 ……….. (3) u ( ∞, y ) = 0, for 0 ≤ y ≤ π ……… (4) u ( 0, y ) = ky, for 0 ≤ y ≤ π ……… (5)Of the three possible solutions of Eq.(1), the solution u ( x, y ) = ( Ae px + Be − px )( C cos py + D sin py ) ………... (6)can satisfy the boundary condition (4). Rewriting (6), we have u ( x, y ) e − px = ( A + Be −2 px )( C cos py + D sin py ) ………. (7)Using boundary condition (4) in (6), we have 26
27. 27. A( C cos py + D sin py ) = 0, for 0 ≤ y ≤ π A=0Using boundary conditions (2) in (6), we have B.C.e = px = 0 for all x > 0 Either B = 0 or C = 0If we assume that B=0, we get a trivial solution C=0Using boundary conditions (3) in (6), we have D sin pπ .Be = py = 0 for all x > 0 B = 0, D = 0 or sin pπ = 0The values B=o and D=0 leads to a trivial solution. sin pπ = 0 p=nWhere n = 0,1,2  ∞Using these values of A, p, C in (6), the solution reduces to u ( x, y ) = λe − nx sin ny , ………. (8)where n = 0,1,2,3 ∞The most general solution of Eq.(1) is ∞ u ( x, y ) = ∑ λn e − nx sin ny ………. (9) n =1Using boundary conditions (5) in (7), we have ∞ ∑λ n sin ny = ky in ( 0, π ) n =1 = ∑ bn sin nyWhich is the Fourier half-range sine series of ky in ( 0, π ) .Comparing like terms in thetwo series, we get. π 2 λ n = bn = ∫ ky sin ny dy π 0 π 2k   − cos ny   − sin ny  =  y −  π   n   n 2  0 2k = ( − 1) n+1 nUsing this value of λ n in (7), the required solution is 27
28. 28. u ( x, y ) = 2 k ∑ ( − 1) n +1 e −nx sin ny n(3) A rectangular plate with insulated surface is 20 cm wide and so long comparedto its width that it may be considered infinite in length without introducing anappreciable error. If the temperature of the short edge x=0 is given by 10 y , for 0 ≤ y ≤ 10 u= 10( 20 − y ) , for 10 ≤ y ≤ 20and the two long edges as well as the other short edge are kept at 0 0 C. Find thesteady state temperature distribution in the plate.Solution:The steady state temperature u ( x, y ) at any point (x, y) of the plate in the steady state isgiven by the equation.. ∂ 2u ∂ 2u + =0 ………… (1) ∂x 2 ∂y 2We have to solve equation (1) satisfying the following boundary conditions. u ( x,0 ) = 0, for x>0 ……… (2) u ( x,20 ) = 0, for x>0 ……….. (3) u ( ∞, y ) = 0, for 0 ≤ y ≤ 20 ……… (4) u ( 0, y ) = f ( y ) , for 0 ≤ y ≤ 20 ……… (5)where 10 y, for 0 ≤ y ≤ 10 f ( y) =  10( 20 − y ) , for 10 ≤ y ≤ 20The most general solution of Eq.(1) is ∞ − nπx nπy u ( x, y ) = ∑ λ n e 20 sin ………. (6) n =1 20Using boundary conditions (5) in (6), we have 28
29. 29. ∞ nπy ∑λ n sin = f ( y ) in ( 0,20 ) n =1 20 nπy = ∑ bn sin 20Which is Fourier half-range sine series of f(y) in ( 0,20)Comparing like terms, we get nπx 20 2.λ n = bn = ∫ f ( x ) sin 20 dy, by Euler ′s formula 20 0 nπy nπy 10 20 = ∫ y sin dy + ∫ ( 20 − y ) sin dy 0 20 10 20 10 20   nπx   nπx    nπy   nπy    − cos   − sin    − cos   − sin    20   20  = y 20  −   + ( 20 − y )  20  − ( − 1)    nπ   n 2π 2     nπ   n 2π 2          20 2  0      20    20   20 2 10   200 nπ 400 nπ   200 nπ 400 nπ  =  − cos + 2 2 sin + cos + 2 2 sin   nπ 2 nπ 2   nπ 2 n π 2  800 nπ = 2 2 sin nπ 2Using this value of λ n in (6), the required solution is u ( x, y ) = 800 ∞ ( − 1) 2 ∑ n +1 π n =1 ( 2n − 1) 2 { } exp − ( 2n − 1)πx sin 20 ( 2n − 1)πy 20(4) A long rectangular plate with insulated surface is 1 cm wide. If the temperaturealong one short edge(y=0) is u ( x,0 ) = k ( 2lx − x 2 ). degrees, for 0<x<l, while the two longedges x=0 and x=l as well as the other short edge are kept at temperature 0 0 C, Findthe steady state temperature function u ( x, y ) .Solution:The steady state temperature u ( x, y ) at any point (x, y) of the plate in the steady state isgiven by the equation.. 29
30. 30. ∂ 2u ∂ 2u + =0 ………… (1) ∂x 2 ∂y 2We have to solve equation (1) satisfying the following boundary conditions. u ( 0, y ) = 0, for y>0 ……… (2) u ( a, y ) = 0, for y>0 ……….. (3) u ( x, ∞ ) = 0, for 0≤ x≤l ……… (4) u ( x,0 ) = k ( lx − x 2 ), for 0 ≤ x ≤ l ……… (5)The most general solution of Eq.(1) is ∞ nπx −nπy l u ( x, y ) = ∑ λn sin .e ………. (6) n =1 lUsing boundary condition (5) in (6), we have nπx = k ( lx − x 2 ), in ( 0, l ) ∞ ∑λ n =1 n sin l ∞ nπx = ∑ bn sin n =1 lWhich is Fourier half-range sine series of k ( 2lx − x 2 ). in ( 0, l ) .Comparing like terms, we get nπx l 2 λ n = bn = ∫ f ( x ) sin dx, by Euler ′s formula l 0 l nπx l ∫ k (lx − x ) sin l dx 2 = 2 l 0 l   nπx   nπx   nπx    − cos   − sin   cos  ( lx − x ) 2k  2  l  − ( l − 2x) l  + ( − 2)  l  = l   nπ   n 2π 2   n 3π 3           l   l2   l 3  0  = 4kl 2 nπ a 3 3 { 1 − ( − 1) n } 0, if n is even  =  8kl 2  3 3 , if n is odd n πUsing this value of λ n in (6), the required solution is 30
31. 31. u ( x, t ) = 8kl 2 π3 ∞ 1 ∑ ( 2n − 1) n =1 3 sin l { ( 2n − 1)πx exp − ( 2n − 1)πy l } UNIT 3 PART A1. Classify the partial differential equation 3u xx + 4u xy + 3u y − 2u x = 0.Ans:Given 3u xx + 4u xy + 3u y − 2u x = 0.A = 3, B = 4, C = 0B 2 − 4 AC =16 > 0, Hyperbolic.2. The ends A and B of a rod of length 10 cm long have their temperature kept at 20 0 Cand 70 0 C. Find the steady state temperature distribution on the rod. 31
32. 32. Ans: When the steady state conditions exists the heat flow equation is ∂ 2u =0 ∂x 2i.e., u ( x) = c1 x + c2 ………………(1)The boundary conditions are (a) u(0) = 20, (b) u(10) = 70Applying (a) in (1), we get u (0) = c2 = 20Substitute this value in (1), we get u ( x ) = c1 x + 20 ………………(2)Applying (b) in (2), we get u (10) = c110 + 20 = 70 ∴ c1 = 5Substitute this value in (2), we get u ( x ) = 5 x + 20 ∂u ∂u3. Solve the equation 3 +2 = 0, given that u ( x,0) = 4e − x by the method of ∂x ∂yseparation of variables.Ans: ∂u ∂uGiven 3 + 2 = 0 ……………….. ∂x ∂y(1)Let u = X(x).Y(y) ……………….(2)Be a solution of (1) ∂u ∂u = X ′Y , = XY ′ ……………… ∂x ∂y(3)Substituting (3) in (1) we get 3 X ′Y + 2 XY ′ = 0 3 X ′ 2Y ′ = =K X Y 3 X ′ − KX = 0, − 2Y ′ − KY = 0 dX dY 3 = KX , 2 = − KY dx dy dX dY 3 = K dx, 2 = − K dy dx dyIntegrating we get 32
33. 33. 3 log X = Kx, 2 log Y = Ky kx ky X =e3, Y =e2 kx kyTherefore u = X .Y = e 3 . e 24. Write the one dimensional wave equation with initial and boundary conditions inwhich the initial position of the string is f (x) and the initial velocity imparted at eachpoint x is g (x) .Ans: ∂2 y ∂2 y The one dimensional wave equation is 2 = α 2 2 ∂t ∂xThe boundary conditions are (i) y(0 , t) = 0 (iii) y(x , 0) = f (x ) ∂y ( x,0) (ii) y(l , t) = 0 (iv) = g ( x) ∂t5. What is the basic difference between the solution of one dimensional wave equationand one dimensional heat equation.Ans: Solution of the one dimensional wave equation is of periodic in nature. Butsolution of the one dimensional heat equation is not of periodic in nature.6. In steady state conditions derive the solution of one dimensional heat flow equation.Ans: When steady state conditions exist the heat floe equation is independent of time t. ∂u ∴ =0 ∂tThe heat flow equation becomes ∂ 2u =0 ∂x 27. What are the possible solutions of one dimensional wave equation.Ans:y ( x , t ) = (C1e px + C2 e − px ) (C3 e pat + C 4 e − pat )y ( x , t ) = (C5 cos px + C6 sin px) (C7 cos pat + C8 sin pat )y ( x , t ) = (C9 x + C10 ) (C11t + C12 ) ∂2 y ∂2 y8. In the wave equation = α 2 2 what does c 2 stand for? ∂t 2 ∂xAns: Tension c2 = T = mass 33
34. 34. 9. State Fourier law of conduction.Ans: The rate at which heat flows across an area A at a distance x from one end of abar given by  ∂u  Q = − KA   ∂x  x  ∂u K is thermal conductivity and   means the temperature gradient at x.  ∂x  x10. What is the constant a 2 in the wave equation utt = a u xx . 2Ans: Tension a2 = mass11. State any two laws which are assumed to derive one dimensional heat equation.Ans: (i) The sides of the bar are insulated so that the loss or gain of heat from the sidesby conduction or radiation is negligible. (ii) The same amount of heat is applied at all points of the face.12. Classify the PDE u xx + xu yy = 0.Ans:Here A = 1, B = x, C = 0 ∴ B 2 − 4 AC = x 2(i) Elliptic if x > 0(ii) Parabolic if x = 0(iii) Hyperbolic if x < 013. Classify the PDE(a) y u xx − 2 xyu xy + x u yy + 2u x − 3u = 0. 2 2 2(b) y u xx + u yy + u x + u y + 7 = 0. 2 2Ans: (a) Here A = y 2 , B = -2xy, C = x 2 ∴ B 2 − 4 AC = 4 x 2 y 2 − 4 x 2 y 2 = 0 ∴ Parabolic (b) Here A = y 2 , B = 0, C = 1. ∴ B 2 − 4 AC = −4 y 2 < 0. ∴ Elliptic.14. An insulated rod of length 60 cm has its ends at A and B maintained at 30 0 C and40 0 C respectively. Find the steady state solution.Ans: 34
35. 35. The heat flow equation is ∂u ∂2 y =α2 2 ……………… ∂t ∂x(1)When the steady state condition exist the heat flow equation becomes ∂ 2u =0 ∂x 2i.e., u ( x) = c1 x + c2 ………………(2)The boundary conditions are (a) u(0) = 30, (b) u(l) = 40Applying (a) in (2), we get u (0) = c2 = 30Substitute this value in (2), we get u ( x) = c1 x + 30 ………………(3)Applying (b) in (3), we get u (10) = c1l + 30 = 40 40 ∴ c1 = lSubstitute this value in (3), we get 40 x u ( x) = x + 30 l15. Solve using separation of variables method yu x + xu y = 0.Ans:Given yu x + xu y = 0. ………………..(1)Let u = X(x).Y(y) ……………….(2)Be a solution of (1) ∂u ∂u = X ′Y , = XY ′ ……………… ∂x ∂y(3)Substituting (3) in (1) we get y. X ′Y + x. XY ′ = 0 X ′ −Y′ = =K xX yY X ′ = KxX , − Y ′ = KyY dX dY = KxX , = − KyY dx dy dX dY = Kx dx, = − Ky dy X Y 35
36. 36. Integrating we get x2 y2 log X = k + k1 , log Y = − k + k2 2 2 kx 2 ky 2 X = c1e 2 , Y = c2 e 2 k 2 − y2 )Therefore u = X .Y = c c e 2 ( x 1 2 PART B(1) A tightly stretched string with fixed end points x=0 and x = l is initially at rest in itsequilibrium position. If it is set vibrating giving each point a velocity λx( l − x ). , thenshow that 8λl 3 ∞ 1 nπx nπat y ( x, t ) = 4 ∑ 4 sin . sin π a n =1,3,5 n l l(2) A rectangular plate is bounded by lines x=0, y=0, x=a, y=b. It’s surface are insulated.The temperature along x=0 and y=o are kept at 0 0 C and others at 100 0 C. Find the steadystate temperature at any point of the plate.(3)A metal bar 10 cm. long, with insulated sides has its ends A and B kept at 20 0 C and40 0 C respectively until steady state conditions prevail. The temperature at A is thensuddenly raised to 50 0 C and at the same instant that at B is lowered to 10 0 C. Find thesubsequent temperature at any point of the bar at any time.(4) A tightly stretched string of length l has its ends fastened at x=0, x = l . The mid-point of the string is mean taken to height ‘b’ and then released from rest in that position.Find the lateral displacement of a point of the string at time‘t’ from the instant of release.(5)If a square plate is bounded by the lines x = ± a and y = ± a and three of its edges arekept at temperature 0 0 C, while the temperature along the edge y=a is kept atu = x + a, − a ≤ x ≤ a, Find the steady state temperature in the plate.(6)A uniform string is stretched and fastened to two points l apart. Motion is started bydisplacing the string into the form of the curve 3  πx  (i) y = k sin   and  l  (ii) y = kx( l − x )and then releasing it from this position at time t=0. Find the displacement of the point ofthe string at a distance x from one end at time t.(7) A long rectangular plate with insulated surface is 1 cm wide. If the temperature alongone short edge(y=0) is u ( x,0 ) = k ( 2lx − x 2 ). degrees, for 0 < x < l , while the two long 36
37. 37. edges x=0 and x=l as well as the other short edge are kept at temperature 0 0 C, Find thesteady state temperature function u ( x, y ) .(8)Find the temperature distribution in a homogeneous bar of length π which is insulatedlaterally, if the ends are kept at zero temperature and if, initially, the temperature is k atthe centre of the bar and falls uniformly to zero at its ends. ∂2 y ∂2 y(9) solve the one dimensional wave equation = a 2 2 in − l ≤ x ≤ l , t ≥ 0, ∂t 2 ∂x ∂ygiven that y ( − l , t ) = 0, y ( l , t ) = 0, ( x,0) = 0 and y ( x,0 ) = ( l − x ). b ∂t l(10) A rectangular plate with insulated surface is 20 cm wide and so long compared to itswidth that it may be considered infinite in length without introducing an appreciableerror. If the temperature of the short edge x=0 is given by 10 y , for 0 ≤ y ≤ 10 u= 10( 20 − y ) , for 10 ≤ y ≤ 20and the two long edges as well as the other short edge are kept at 0 0 C. Find the steadystate temperature distribution in the plate.(11) Solve the one dimensional heat flow equation ∂u ∂ 2u =α2 2 ∂t ∂xSatisfying the following boundary conditions. ∂u (i) ( 0, t ) = 0, for all t ≥ 0 ∂x ∂u (ii) ( π , t ) = 0, for all t ≥ 0 ∂x (iii) u ( x,0 ) = cos 2 x, for 0 < x < π(12)A rectangular plane with insulated surface is a cm wide and so long compared to itswidth that it may be considered infinite in length without introducing an appreciableerror. If the two long edges x=0 and x=a and the short edge at infinity are kept attemperature 0 0 C, while the other short edge y=0 is kept at temperature 3 πx(i) u 0 sin and (ii) T (constant). Find the steady state temperature at any point a(x, y) of the plate. 37
38. 38. (13) A tightly stretched strings with fixed end points x=0 and x=50 is initially at rest in itsequilibrium position. If it is said to vibrate by giving each point a velocity 3 πx(i) v = v 0 sin and 50 πx 2πx(ii) v = v 0 sin cos , 50 50Find the displacement of any point of the string at any subsequent time.(14) An infinitely long metal plate in the form of an area is enclosed between the lines y = 0 and y = π for positive values of x. The temperature is zero along the edges y = 0 , y = π and the edge at infinity. If the edge x=0 is kept at temperature ky, Find the steady state temperature distribution in the plate.(15) A taut string of length 2l , fastened at both ends, is disturbed from its position ofequilibrium by imparting to each of its points an initial velocity of magnitude k ( 2lx − x 2 ).Find the displacement function y ( x, t ) 38