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Section A: Long Answer Questions

Attempt all questions.

5 questions
1long8 marks

State Green's theorem in the plane. Hence verify Green's theorem for the line integral

C[(3x28y2)dx+(4y6xy)dy]\oint_C \left[(3x^2 - 8y^2)\,dx + (4y - 6xy)\,dy\right]

where CC is the boundary of the region bounded by the lines x=0x = 0, y=0y = 0 and x+y=1x + y = 1, traversed counter-clockwise.

Statement of Green's theorem. If CC is a positively oriented, piecewise-smooth, simple closed curve in the plane enclosing a region RR, and M(x,y)M(x,y), N(x,y)N(x,y) together with their first partial derivatives are continuous on RR, then

C(Mdx+Ndy)=R(NxMy)dA.\oint_C (M\,dx + N\,dy) = \iint_R \left(\frac{\partial N}{\partial x} - \frac{\partial M}{\partial y}\right)\,dA.

Here M=3x28y2M = 3x^2 - 8y^2 and N=4y6xyN = 4y - 6xy.

Right-hand side (double integral).

Nx=6y,My=16y,\frac{\partial N}{\partial x} = -6y, \qquad \frac{\partial M}{\partial y} = -16y, NxMy=6y(16y)=10y.\frac{\partial N}{\partial x} - \frac{\partial M}{\partial y} = -6y - (-16y) = 10y.

The region RR is the triangle with vertices (0,0)(0,0), (1,0)(1,0), (0,1)(0,1). For fixed x[0,1]x \in [0,1], yy runs from 00 to 1x1-x:

R10ydA=0101x10ydydx=0110(1x)22dx=501(1x)2dx.\iint_R 10y\,dA = \int_0^1 \int_0^{1-x} 10y\,dy\,dx = \int_0^1 10\cdot\frac{(1-x)^2}{2}\,dx = 5\int_0^1 (1-x)^2\,dx.

With 01(1x)2dx=13\int_0^1 (1-x)^2\,dx = \tfrac13, RHS =513=53= 5 \cdot \tfrac13 = \dfrac{5}{3}.

Left-hand side (line integral). CC has three pieces, counter-clockwise.

Segment C1C_1: (0,0)(1,0)(0,0)\to(1,0) along y=0y=0, dy=0dy=0, x:01x: 0\to1.

C1(3x20)dx=013x2dx=1.\int_{C_1} (3x^2 - 0)\,dx = \int_0^1 3x^2\,dx = 1.

Segment C2C_2: (1,0)(0,1)(1,0)\to(0,1) along x+y=1x+y=1. Parametrize x=1tx = 1-t, y=ty = t, t:01t:0\to1, so dx=dtdx=-dt, dy=dtdy=dt.

  • M=3(1t)28t2M = 3(1-t)^2 - 8t^2, N=4t6(1t)tN = 4t - 6(1-t)t.
C2=01[(3(1t)28t2)(1)+(4t6(1t)t)(1)]dt.\int_{C_2} = \int_0^1 \Big[(3(1-t)^2 - 8t^2)(-1) + (4t - 6(1-t)t)(1)\Big]dt.

Expand: 3(1t)2=36t+3t23(1-t)^2 = 3 - 6t + 3t^2, so M=36t+3t28t2=36t5t2M = 3 - 6t + 3t^2 - 8t^2 = 3 - 6t - 5t^2; M=3+6t+5t2-M = -3 + 6t + 5t^2. N=4t6t+6t2=2t+6t2N = 4t - 6t + 6t^2 = -2t + 6t^2. Integrand =(3+6t+5t2)+(2t+6t2)=3+4t+11t2= (-3 + 6t + 5t^2) + (-2t + 6t^2) = -3 + 4t + 11t^2.

01(3+4t+11t2)dt=3+2+113=1+113=83.\int_0^1 (-3 + 4t + 11t^2)\,dt = -3 + 2 + \tfrac{11}{3} = -1 + \tfrac{11}{3} = \tfrac{8}{3}.

Segment C3C_3: (0,1)(0,0)(0,1)\to(0,0) along x=0x=0, dx=0dx=0, y:10y:1\to0.

C3(4y0)dy=104ydy=[2y2]10=2.\int_{C_3} (4y - 0)\,dy = \int_1^0 4y\,dy = \big[2y^2\big]_1^0 = -2.

Total line integral =1+832=1+83=53.= 1 + \tfrac{8}{3} - 2 = -1 + \tfrac{8}{3} = \dfrac{5}{3}.

Since LHS =53== \dfrac{5}{3} = RHS, Green's theorem is verified.

line-integralgreens-theoremvector-calculus
2long8 marks

State the divergence theorem (Gauss's theorem). Using it, evaluate the surface integral

SFndS,F=2xi+3yj+z2k,\iint_S \mathbf{F}\cdot \mathbf{n}\,dS, \qquad \mathbf{F} = 2x\,\mathbf{i} + 3y\,\mathbf{j} + z^2\,\mathbf{k},

where SS is the closed surface of the cube bounded by x=0x=0, x=2x=2, y=0y=0, y=2y=2, z=0z=0, z=2z=2, with n\mathbf{n} the outward unit normal.

Statement of the divergence theorem. If VV is a solid region bounded by a closed, piecewise-smooth, outward-oriented surface SS, and F\mathbf{F} is a vector field with continuous first partial derivatives on VV, then

SFndS=V(F)dV.\iint_S \mathbf{F}\cdot\mathbf{n}\,dS = \iiint_V (\nabla\cdot\mathbf{F})\,dV.

Compute the divergence.

F=x(2x)+y(3y)+z(z2)=2+3+2z=5+2z.\nabla\cdot\mathbf{F} = \frac{\partial}{\partial x}(2x) + \frac{\partial}{\partial y}(3y) + \frac{\partial}{\partial z}(z^2) = 2 + 3 + 2z = 5 + 2z.

Evaluate the volume integral over the cube 0x,y,z20\le x,y,z\le 2:

V(5+2z)dV=02 ⁣02 ⁣02(5+2z)dzdydx.\iiint_V (5 + 2z)\,dV = \int_0^2\!\int_0^2\!\int_0^2 (5 + 2z)\,dz\,dy\,dx.

The integrand does not depend on xx or yy, so the xx and yy integrations each give a factor of 22 (area =2×2=4= 2\times2 = 4):

=402(5+2z)dz=4[5z+z2]02=4(10+4)=414=56.= 4\int_0^2 (5 + 2z)\,dz = 4\big[5z + z^2\big]_0^2 = 4\,(10 + 4) = 4\cdot 14 = 56.

Final answer: SFndS=56.\displaystyle \iint_S \mathbf{F}\cdot\mathbf{n}\,dS = \mathbf{56}.

Check by direct face integration (optional). Outflux contributions:

  • x=2x=2 face: FxdA=2(2)4=16\int F_x\,dA = 2(2)\cdot 4 = 16; x=0x=0 face: Fx=00F_x=0 \Rightarrow 0.
  • y=2y=2 face: 3(2)4=243(2)\cdot 4 = 24; y=0y=0: 00.
  • z=2z=2 face: z2=444=16z^2 = 4 \Rightarrow 4\cdot 4 = 16; z=0z=0: 00. Sum =16+24+16=56.= 16 + 24 + 16 = 56. Confirms the result.
divergence-theoremsurface-integralvector-calculus
3long8 marks

Using the Laplace transform method, solve the initial value problem

y+4y+3y=6e2t,y(0)=1,y(0)=1.y'' + 4y' + 3y = 6e^{-2t}, \qquad y(0) = 1, \quad y'(0) = -1.

Apply the Laplace transform. Let Y(s)=L{y(t)}Y(s) = \mathcal{L}\{y(t)\}. Using

L{y}=sYy(0),L{y}=s2Ysy(0)y(0),\mathcal{L}\{y'\} = sY - y(0), \qquad \mathcal{L}\{y''\} = s^2 Y - s\,y(0) - y'(0),

and L{e2t}=1s+2\mathcal{L}\{e^{-2t}\} = \dfrac{1}{s+2}:

[s2Ys(1)(1)]+4[sY1]+3Y=6s+2.\big[s^2 Y - s(1) - (-1)\big] + 4\big[sY - 1\big] + 3Y = \frac{6}{s+2}.

Collect terms:

(s2+4s+3)Ys+14=6s+2,(s^2 + 4s + 3)Y - s + 1 - 4 = \frac{6}{s+2}, (s2+4s+3)Y=6s+2+s+3.(s^2 + 4s + 3)Y = \frac{6}{s+2} + s + 3.

Note s2+4s+3=(s+1)(s+3)s^2 + 4s + 3 = (s+1)(s+3). Thus

Y=6(s+2)(s+1)(s+3)+s+3(s+1)(s+3)=6(s+1)(s+2)(s+3)+1s+1.Y = \frac{6}{(s+2)(s+1)(s+3)} + \frac{s+3}{(s+1)(s+3)} = \frac{6}{(s+1)(s+2)(s+3)} + \frac{1}{s+1}.

Partial fractions for the first term. Write

6(s+1)(s+2)(s+3)=As+1+Bs+2+Cs+3.\frac{6}{(s+1)(s+2)(s+3)} = \frac{A}{s+1} + \frac{B}{s+2} + \frac{C}{s+3}.
  • AA: set s=1s=-1: A=6(1)(2)=3.A = \dfrac{6}{(1)(2)} = 3.
  • BB: set s=2s=-2: B=6(1)(1)=6.B = \dfrac{6}{(-1)(1)} = -6.
  • CC: set s=3s=-3: C=6(2)(1)=3.C = \dfrac{6}{(-2)(-1)} = 3. So
Y=3s+16s+2+3s+3+1s+1=4s+16s+2+3s+3.Y = \frac{3}{s+1} - \frac{6}{s+2} + \frac{3}{s+3} + \frac{1}{s+1} = \frac{4}{s+1} - \frac{6}{s+2} + \frac{3}{s+3}.

Inverse transform, using L1{1/(s+a)}=eat\mathcal{L}^{-1}\{1/(s+a)\} = e^{-at}:

y(t)=4et6e2t+3e3t.\boxed{\,y(t) = 4e^{-t} - 6e^{-2t} + 3e^{-3t}\,}.

Check initial conditions. y(0)=46+3=1.y(0) = 4 - 6 + 3 = 1.y(t)=4et+12e2t9e3ty'(t) = -4e^{-t} + 12e^{-2t} - 9e^{-3t}, so y(0)=4+129=1.y'(0) = -4 + 12 - 9 = -1.

laplace-transforminitial-value-problemdifferential-equations
4long8 marks

State Cauchy's residue theorem. Using it, evaluate

Cz2+1z22zdz,\oint_C \frac{z^2 + 1}{z^2 - 2z}\,dz,

where CC is the circle z=3|z| = 3 described counter-clockwise.

Cauchy's residue theorem. If f(z)f(z) is analytic inside and on a simple closed contour CC except at a finite number of isolated singular points z1,z2,,znz_1, z_2, \dots, z_n inside CC, then

Cf(z)dz=2πik=1nResz=zkf(z).\oint_C f(z)\,dz = 2\pi i \sum_{k=1}^{n} \operatorname{Res}_{z=z_k} f(z).

Identify singularities. f(z)=z2+1z22z=z2+1z(z2)f(z) = \dfrac{z^2 + 1}{z^2 - 2z} = \dfrac{z^2 + 1}{z(z-2)}. Simple poles at z=0z = 0 and z=2z = 2. Both satisfy z<3|z| < 3, so both lie inside CC.

Residue at z=0z = 0 (simple pole):

Resz=0f=limz0zz2+1z(z2)=0+102=12.\operatorname{Res}_{z=0} f = \lim_{z\to 0} z\cdot \frac{z^2+1}{z(z-2)} = \frac{0+1}{0-2} = -\frac{1}{2}.

Residue at z=2z = 2 (simple pole):

Resz=2f=limz2(z2)z2+1z(z2)=4+12=52.\operatorname{Res}_{z=2} f = \lim_{z\to 2} (z-2)\cdot \frac{z^2+1}{z(z-2)} = \frac{4+1}{2} = \frac{5}{2}.

Apply the theorem.

Cf(z)dz=2πi(12+52)=2πi2=4πi.\oint_C f(z)\,dz = 2\pi i \left(-\frac{1}{2} + \frac{5}{2}\right) = 2\pi i \cdot 2 = \mathbf{4\pi i}.

Remark. Since deg(num)=deg(den)\deg(\text{num}) = \deg(\text{den}), one could also write f(z)=1+2z+1z(z2)f(z) = 1 + \frac{2z+1}{z(z-2)}; the constant 11 integrates to 00 around the closed contour, and the remaining proper fraction gives the same residue sum.

complex-analysiscauchy-residue-theoremcontour-integration
5long8 marks

A string of length L=πL = \pi is stretched and fastened at both ends. It is set vibrating from rest with initial displacement u(x,0)=3sinxsin3xu(x,0) = 3\sin x - \sin 3x. The transverse displacement satisfies the wave equation

2ut2=c22ux2,0<x<π,\frac{\partial^2 u}{\partial t^2} = c^2\frac{\partial^2 u}{\partial x^2}, \qquad 0 < x < \pi,

with u(0,t)=u(π,t)=0u(0,t) = u(\pi,t) = 0 and ut(x,0)=0u_t(x,0) = 0. Using separation of variables, find u(x,t)u(x,t).

Separation of variables. Seek u(x,t)=X(x)T(t)u(x,t) = X(x)T(t). Substituting into utt=c2uxxu_{tt} = c^2 u_{xx} and dividing by c2XTc^2 XT:

Tc2T=XX=λ  (constant).\frac{T''}{c^2 T} = \frac{X''}{X} = -\lambda \;(\text{constant}).

This gives X+λX=0X'' + \lambda X = 0 and T+λc2T=0T'' + \lambda c^2 T = 0.

Boundary conditions. u(0,t)=u(π,t)=0X(0)=X(π)=0u(0,t)=u(\pi,t)=0 \Rightarrow X(0)=X(\pi)=0. Non-trivial solutions require λ=n2\lambda = n^2 (n=1,2,3,n = 1,2,3,\dots) with

Xn(x)=sin(nx).X_n(x) = \sin(nx).

Time part. With λ=n2\lambda = n^2, T+n2c2T=0Tn(t)=Ancos(nct)+Bnsin(nct)T'' + n^2 c^2 T = 0 \Rightarrow T_n(t) = A_n\cos(nct) + B_n\sin(nct).

Apply the initial velocity condition. ut(x,0)=0u_t(x,0) = 0 for all xx forces Bn=0B_n = 0 for every nn. Hence the general solution is

u(x,t)=n=1Ancos(nct)sin(nx).u(x,t) = \sum_{n=1}^{\infty} A_n \cos(nct)\sin(nx).

Apply the initial displacement. At t=0t=0:

u(x,0)=n=1Ansin(nx)=3sinxsin3x.u(x,0) = \sum_{n=1}^{\infty} A_n \sin(nx) = 3\sin x - \sin 3x.

Matching coefficients term by term (the right side is already a finite sine series):

A1=3,A3=1,An=0 otherwise.A_1 = 3, \qquad A_3 = -1, \qquad A_n = 0 \text{ otherwise}.

Final solution.

u(x,t)=3cos(ct)sinxcos(3ct)sin3x.\boxed{\,u(x,t) = 3\cos(ct)\sin x - \cos(3ct)\sin 3x\,}.

Verification. Each term satisfies the wave equation: for un=cos(nct)sin(nx)u_n = \cos(nct)\sin(nx), utt=n2c2unu_{tt} = -n^2c^2 u_n and c2uxx=n2c2unc^2 u_{xx} = -n^2 c^2 u_n, so utt=c2uxxu_{tt} = c^2 u_{xx}. At t=0t=0: u=3sinxsin3xu = 3\sin x - \sin 3x ✓ and ut=3csin(ct)sinx+3csin(3ct)sin3xt=0=0u_t = -3c\sin(ct)\sin x + 3c\sin(3ct)\sin 3x \big|_{t=0} = 0 ✓; boundaries vanish since sin(0)=sin(nπ)=0\sin(0)=\sin(n\pi)=0 ✓.

partial-differential-equationswave-equationseparation-of-variables
B

Section B: Short Answer Questions

Attempt all questions.

6 questions
6short7 marks

Evaluate the double integral by changing the order of integration:

01x1ey2dydx.\int_0^1 \int_{x}^{1} e^{y^2}\,dy\,dx.

Identify the region. The inner limits give xy1x \le y \le 1 and the outer give 0x10 \le x \le 1. So the region is

R={(x,y):0x1,  xy1},R = \{(x,y): 0\le x\le 1,\; x\le y\le 1\},

the triangle with vertices (0,0)(0,0), (0,1)(0,1), (1,1)(1,1).

Reason for changing order. ey2dy\int e^{y^2}\,dy has no elementary antiderivative, so integrate in xx first.

Re-describe RR with yy outer. For fixed y[0,1]y\in[0,1], xx runs from 00 to yy (since xyx\le y):

R={(x,y):0y1,  0xy}.R = \{(x,y): 0\le y\le 1,\; 0\le x\le y\}.

Thus

I=010yey2dxdy.I = \int_0^1 \int_0^{y} e^{y^2}\,dx\,dy.

Inner integral (over xx, ey2e^{y^2} constant in xx):

0yey2dx=ey2y.\int_0^{y} e^{y^2}\,dx = e^{y^2}\cdot y.

Outer integral. Substitute w=y2w = y^2, dw=2ydydw = 2y\,dy:

I=01yey2dy=1201ewdw=12[ew]01=12(e1).I = \int_0^1 y\,e^{y^2}\,dy = \frac{1}{2}\int_0^1 e^{w}\,dw = \frac{1}{2}\big[e^{w}\big]_0^1 = \frac{1}{2}(e - 1).

Final answer: I=e120.8591.\displaystyle I = \frac{e-1}{2} \approx \mathbf{0.8591}.

double-integralchange-of-ordermultiple-integral
7short7 marks

Given the scalar field ϕ(x,y,z)=x2y+y2z+z2x\phi(x,y,z) = x^2 y + y^2 z + z^2 x, at the point P(1,1,2)P(1, -1, 2): (a) find ϕ\nabla\phi; (b) find the directional derivative of ϕ\phi at PP in the direction of the vector a=2ij+2k\mathbf{a} = 2\mathbf{i} - \mathbf{j} + 2\mathbf{k}; (c) state the maximum rate of change of ϕ\phi at PP.

(a) Gradient.

ϕ=(ϕx,ϕy,ϕz)=(2xy+z2,  x2+2yz,  y2+2zx).\nabla\phi = \left(\frac{\partial\phi}{\partial x},\frac{\partial\phi}{\partial y},\frac{\partial\phi}{\partial z}\right) = (2xy + z^2,\; x^2 + 2yz,\; y^2 + 2zx).

At P(1,1,2)P(1,-1,2):

  • ϕx=2(1)(1)+22=2+4=2\phi_x = 2(1)(-1) + 2^2 = -2 + 4 = 2
  • ϕy=12+2(1)(2)=14=3\phi_y = 1^2 + 2(-1)(2) = 1 - 4 = -3
  • ϕz=(1)2+2(2)(1)=1+4=5\phi_z = (-1)^2 + 2(2)(1) = 1 + 4 = 5
ϕP=2i3j+5k.\nabla\phi\big|_P = 2\mathbf{i} - 3\mathbf{j} + 5\mathbf{k}.

(b) Directional derivative. Unit vector along a=(2,1,2)\mathbf{a} = (2,-1,2): a=4+1+4=3|\mathbf{a}| = \sqrt{4+1+4} = 3, so a^=13(2,1,2)\hat{\mathbf{a}} = \tfrac13(2,-1,2).

Da^ϕ=ϕa^=(2)(2)+(3)(1)+(5)(2)3=4+3+103=173.D_{\hat{\mathbf{a}}}\phi = \nabla\phi\cdot\hat{\mathbf{a}} = \frac{(2)(2) + (-3)(-1) + (5)(2)}{3} = \frac{4 + 3 + 10}{3} = \frac{17}{3}. Da^ϕ=1735.667.D_{\hat{\mathbf{a}}}\phi = \frac{17}{3} \approx \mathbf{5.667}.

(c) Maximum rate of change. This equals ϕ|\nabla\phi| at PP:

ϕ=22+(3)2+52=4+9+25=386.164,|\nabla\phi| = \sqrt{2^2 + (-3)^2 + 5^2} = \sqrt{4 + 9 + 25} = \sqrt{38} \approx \mathbf{6.164},

attained in the direction of ϕ=2i3j+5k\nabla\phi = 2\mathbf{i} - 3\mathbf{j} + 5\mathbf{k}.

vector-calculusgradientdirectional-derivative
8short7 marks

Find the inverse Laplace transform

L1{s(s2+1)(s2+4)}\mathcal{L}^{-1}\left\{\frac{s}{(s^2 + 1)(s^2 + 4)}\right\}

using partial fractions. Verify the result is consistent at t=0t = 0.

Partial fractions. Since the numerator ss is odd, write

s(s2+1)(s2+4)=As+Bs2+1+Cs+Ds2+4.\frac{s}{(s^2+1)(s^2+4)} = \frac{As + B}{s^2+1} + \frac{Cs + D}{s^2+4}.

Multiply through:

s=(As+B)(s2+4)+(Cs+D)(s2+1).s = (As+B)(s^2+4) + (Cs+D)(s^2+1).

Expand:

s=(A+C)s3+(B+D)s2+(4A+C)s+(4B+D).s = (A+C)s^3 + (B+D)s^2 + (4A + C)s + (4B + D).

Match coefficients:

  • s3s^3: A+C=0A + C = 0
  • s2s^2: B+D=0B + D = 0
  • s1s^1: 4A+C=14A + C = 1
  • s0s^0: 4B+D=04B + D = 0

From A+C=0C=AA + C = 0 \Rightarrow C = -A. Then 4AA=13A=1A=134A - A = 1 \Rightarrow 3A = 1 \Rightarrow A = \tfrac13, C=13C = -\tfrac13. From B+D=0B + D = 0 and 4B+D=04B + D = 0: subtract to get 3B=0B=03B = 0 \Rightarrow B = 0, D=0D = 0.

So

s(s2+1)(s2+4)=13ss2+113ss2+4.\frac{s}{(s^2+1)(s^2+4)} = \frac{1}{3}\cdot\frac{s}{s^2+1} - \frac{1}{3}\cdot\frac{s}{s^2+4}.

Inverse transform, using L1{s/(s2+a2)}=cos(at)\mathcal{L}^{-1}\{s/(s^2+a^2)\} = \cos(at):

L1{s(s2+1)(s2+4)}=13cost13cos2t=13(costcos2t).\mathcal{L}^{-1}\left\{\frac{s}{(s^2+1)(s^2+4)}\right\} = \frac{1}{3}\cos t - \frac{1}{3}\cos 2t = \frac{1}{3}(\cos t - \cos 2t).

Final answer: f(t)=13(costcos2t).\displaystyle f(t) = \frac{1}{3}\big(\cos t - \cos 2t\big).

Consistency at t=0t=0. f(0)=13(11)=0f(0) = \tfrac13(1 - 1) = 0. By the initial value theorem, limssF(s)=limss2(s2+1)(s2+4)=0\lim_{s\to\infty} sF(s) = \lim_{s\to\infty}\frac{s^2}{(s^2+1)(s^2+4)} = 0, which matches f(0)=0f(0)=0. ✓

laplace-transformconvolutioninverse-transform
9short6 marks

Find the Fourier cosine transform of the function

f(x)={1,0x<a0,xa,f(x) = \begin{cases} 1, & 0 \le x < a \\ 0, & x \ge a, \end{cases}

and hence write down f(x)f(x) in terms of its cosine integral representation.

Definition. The Fourier cosine transform is

Fc(ω)=2π0f(x)cos(ωx)dx.F_c(\omega) = \sqrt{\frac{2}{\pi}}\int_0^{\infty} f(x)\cos(\omega x)\,dx.

Compute the transform. Since f(x)=1f(x) = 1 on [0,a)[0,a) and 00 beyond:

Fc(ω)=2π0acos(ωx)dx=2π[sin(ωx)ω]0a=2πsin(ωa)ω.F_c(\omega) = \sqrt{\frac{2}{\pi}}\int_0^{a} \cos(\omega x)\,dx = \sqrt{\frac{2}{\pi}}\left[\frac{\sin(\omega x)}{\omega}\right]_0^{a} = \sqrt{\frac{2}{\pi}}\,\frac{\sin(\omega a)}{\omega}.

So

Fc(ω)=2πsin(aω)ω,ω>0.F_c(\omega) = \sqrt{\frac{2}{\pi}}\,\frac{\sin(a\omega)}{\omega}, \qquad \omega > 0.

Inversion (cosine integral representation). The inverse cosine transform is

f(x)=2π0Fc(ω)cos(ωx)dω=2π0sin(aω)ωcos(ωx)dω.f(x) = \sqrt{\frac{2}{\pi}}\int_0^{\infty} F_c(\omega)\cos(\omega x)\,d\omega = \frac{2}{\pi}\int_0^{\infty}\frac{\sin(a\omega)}{\omega}\cos(\omega x)\,d\omega.

Thus

2π0sin(aω)cos(ωx)ωdω={1,0x<a12,x=a0,x>a,\frac{2}{\pi}\int_0^{\infty}\frac{\sin(a\omega)\cos(\omega x)}{\omega}\,d\omega = \begin{cases} 1, & 0 \le x < a \\ \tfrac12, & x = a \\ 0, & x > a, \end{cases}

where the value 12\tfrac12 at x=ax=a is the average of the left and right limits at the jump discontinuity (Dirichlet condition).

fourier-transformfourier-integraltransforms
10short6 marks

Show that the function u(x,y)=x33xy2+2yu(x,y) = x^3 - 3xy^2 + 2y is harmonic, and find its harmonic conjugate v(x,y)v(x,y) so that f(z)=u+ivf(z) = u + iv is analytic. Express f(z)f(z) as a function of zz.

Check harmonicity. Compute second partials of u=x33xy2+2yu = x^3 - 3xy^2 + 2y:

ux=3x23y2,uxx=6x,uy=6xy+2,uyy=6x.u_x = 3x^2 - 3y^2, \quad u_{xx} = 6x, \qquad u_y = -6xy + 2, \quad u_{yy} = -6x.

Then uxx+uyy=6x6x=0u_{xx} + u_{yy} = 6x - 6x = 0, so uu satisfies Laplace's equation and is harmonic.

Find the conjugate via Cauchy–Riemann. For f=u+ivf = u + iv analytic: vy=uxv_y = u_x and vx=uyv_x = -u_y.

From vy=ux=3x23y2v_y = u_x = 3x^2 - 3y^2, integrate with respect to yy:

v=3x2yy3+g(x),v = 3x^2 y - y^3 + g(x),

where g(x)g(x) is an arbitrary function of xx.

Differentiate w.r.t. xx: vx=6xy+g(x)v_x = 6xy + g'(x). The second CR equation requires

vx=uy=(6xy+2)=6xy2.v_x = -u_y = -(-6xy + 2) = 6xy - 2.

Matching: 6xy+g(x)=6xy2g(x)=2g(x)=2x+C.6xy + g'(x) = 6xy - 2 \Rightarrow g'(x) = -2 \Rightarrow g(x) = -2x + C.

Thus (taking C=0C = 0)

v(x,y)=3x2yy32x.v(x,y) = 3x^2 y - y^3 - 2x.

Form f(z)f(z).

f=u+iv=(x33xy2+2y)+i(3x2yy32x).f = u + iv = (x^3 - 3xy^2 + 2y) + i(3x^2 y - y^3 - 2x).

Group the cubic terms: x33xy2+i(3x2yy3)=(x+iy)3=z3x^3 - 3xy^2 + i(3x^2 y - y^3) = (x+iy)^3 = z^3. Group the linear terms: 2y2ix=2i(x+iy)=2iz2y - 2ix = -2i(x + iy) = -2iz (since 2iiy=2y-2i\cdot iy = 2y and 2ix=2ix-2i\cdot x = -2ix). Therefore

f(z)=z32iz+C,C a real constant (take C=0).\boxed{\,f(z) = z^3 - 2iz + C\,}, \quad C \text{ a real constant (take } C=0).
complex-analysiscauchy-riemannanalytic-function
11short7 marks

Form the partial differential equation by eliminating the arbitrary constants aa and bb from

z=(x2+a)(y2+b).z = (x^2 + a)(y^2 + b).

Also, classify the second-order PDE uxx+4uxy+4uyy=0u_{xx} + 4u_{xy} + 4u_{yy} = 0 as elliptic, parabolic or hyperbolic, giving reasons.

Part 1 — Eliminate aa and bb. Given z=(x2+a)(y2+b)z = (x^2 + a)(y^2 + b).

Differentiate partially:

p=zx=2x(y2+b),q=zy=2y(x2+a).p = \frac{\partial z}{\partial x} = 2x(y^2 + b), \qquad q = \frac{\partial z}{\partial y} = 2y(x^2 + a).

From these,

y2+b=p2x,x2+a=q2y.y^2 + b = \frac{p}{2x}, \qquad x^2 + a = \frac{q}{2y}.

Substitute into z=(x2+a)(y2+b)z = (x^2+a)(y^2+b):

z=q2yp2x=pq4xy.z = \frac{q}{2y}\cdot\frac{p}{2x} = \frac{pq}{4xy}.

Therefore the required PDE is

4xyz=pq,i.e. 4xyz=zxzy.\boxed{\,4xyz = pq\,}, \qquad \text{i.e. } 4xy\,z = \frac{\partial z}{\partial x}\frac{\partial z}{\partial y}.

Part 2 — Classification. A second-order linear PDE Auxx+Buxy+Cuyy+=0A u_{xx} + B u_{xy} + C u_{yy} + \dots = 0 is classified by the discriminant B24ACB^2 - 4AC:

  • B24AC<0B^2 - 4AC < 0 → elliptic,
  • B24AC=0B^2 - 4AC = 0 → parabolic,
  • B24AC>0B^2 - 4AC > 0 → hyperbolic.

For uxx+4uxy+4uyy=0u_{xx} + 4u_{xy} + 4u_{yy} = 0: A=1A = 1, B=4B = 4, C=4C = 4.

B24AC=164(1)(4)=1616=0.B^2 - 4AC = 16 - 4(1)(4) = 16 - 16 = 0.

Since the discriminant is 00, the PDE is parabolic (everywhere in the plane).

partial-differential-equationsheat-equationboundary-value-problem

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