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Section A: Long Answer Questions

Attempt all questions.

5 questions
1long8 marks

State Green's theorem in the plane. Using Green's theorem, evaluate the line integral

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

where CC is the boundary of the region bounded by the parabola y=xy = \sqrt{x} and the line y=xy = x, traversed counterclockwise.

Green's theorem. If CC is a positively oriented, piecewise-smooth, simple closed curve enclosing a region RR in the plane, and P(x,y)P(x,y), Q(x,y)Q(x,y) have continuous first partial derivatives on RR, then

CPdx+Qdy=R(QxPy)dA.\oint_C P\,dx + Q\,dy = \iint_R \left(\frac{\partial Q}{\partial x} - \frac{\partial P}{\partial y}\right)\,dA.

Identify PP and QQ.

P=3x28y2,Q=4y6xy.P = 3x^2 - 8y^2,\qquad Q = 4y - 6xy.

Compute partials.

Qx=6y,Py=16y.\frac{\partial Q}{\partial x} = -6y,\qquad \frac{\partial P}{\partial y} = -16y. QxPy=6y(16y)=10y.\frac{\partial Q}{\partial x} - \frac{\partial P}{\partial y} = -6y - (-16y) = 10y.

Region of integration. The curves y=xy=\sqrt{x} and y=xy=x meet where x=xx=x2x(x1)=0\sqrt{x}=x \Rightarrow x = x^2 \Rightarrow x(x-1)=0, i.e. at x=0x=0 and x=1x=1. On 0x10\le x\le 1, xx\sqrt{x}\ge x, so the region is

R:0x1,xyx.R: \quad 0 \le x \le 1,\qquad x \le y \le \sqrt{x}.
 y
 1 +        * (1,1)
   |     .' /
   |   .'  /   y = sqrt(x) (upper)
   | .'   /    y = x       (lower)
 0 +-----+----- x
   0     1

Set up the double integral.

R10ydA=01xx10ydydx.\iint_R 10y\,dA = \int_0^1 \int_x^{\sqrt{x}} 10y\,dy\,dx.

Inner integral:

xx10ydy=10y22xx=5[(x)2x2]=5(xx2).\int_x^{\sqrt{x}} 10y\,dy = 10\cdot\frac{y^2}{2}\Big|_x^{\sqrt{x}} = 5\left[(\sqrt{x})^2 - x^2\right] = 5\left(x - x^2\right).

Outer integral:

015(xx2)dx=5[x22x33]01=5(1213)=516=56.\int_0^1 5\left(x - x^2\right)\,dx = 5\left[\frac{x^2}{2} - \frac{x^3}{3}\right]_0^1 = 5\left(\frac{1}{2} - \frac{1}{3}\right) = 5\cdot\frac{1}{6} = \frac{5}{6}.

Result.

CPdx+Qdy=560.8333\boxed{\oint_C P\,dx + Q\,dy = \dfrac{5}{6} \approx 0.8333}
line-integralgreens-theoremvector-calculus
2long8 marks

State the Divergence (Gauss) theorem. Use it to evaluate SFndS\displaystyle \iint_S \mathbf{F}\cdot \mathbf{n}\,dS for the vector field

F=2xi+3yj+z2k,\mathbf{F} = 2x\,\mathbf{i} + 3y\,\mathbf{j} + z^2\,\mathbf{k},

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

Divergence theorem. For a vector field F\mathbf{F} with continuous partial derivatives on a solid region VV bounded by the closed surface SS (outward normal n\mathbf{n}),

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.

Set up the volume integral over the cube 0x2, 0y2, 0z20\le x\le 2,\ 0\le y\le 2,\ 0\le z\le 2:

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

The integrand does not depend on xx or yy, so integrating over xx and yy gives a factor 2×2=42\times 2 = 4:

=402(5+2z)dz.= 4\int_0^2 (5 + 2z)\,dz.

Evaluate the zz-integral:

02(5+2z)dz=[5z+z2]02=(10+4)0=14.\int_0^2 (5 + 2z)\,dz = \left[5z + z^2\right]_0^2 = (10 + 4) - 0 = 14.

Therefore

SFndS=4×14=56.\iint_S \mathbf{F}\cdot \mathbf{n}\,dS = 4 \times 14 = 56.

Check (direct, face-by-face). Flux through each pair of opposite faces:

  • xx-faces: at x=2x=2, flux = ⁣2(2)dydz=44=16=\int\!\int 2(2)\,dy\,dz = 4\cdot4=16; at x=0x=0, 2(0)=02(0)=0 outward (x)(-x) contributes 00. Net =16=16.
  • yy-faces: at y=2y=2, 3(2)=63(2)=6, flux =64=24=6\cdot4=24; at y=0y=0, 00. Net =24=24.
  • zz-faces: at z=2z=2, z2=4z^2=4, flux =44=16=4\cdot4=16; at z=0z=0, 00. Net =16=16.

Total =16+24+16=56=16+24+16 = 56, confirming the answer.

Result.

SFndS=56\boxed{\iint_S \mathbf{F}\cdot \mathbf{n}\,dS = 56}
divergence-theoremsurface-integralvector-calculus
3long8 marks

Using the Laplace transform, solve the initial value problem

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

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

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

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

[s2Ys(1)0]+4[sY1]+3Y=1s+2.\left[s^2 Y - s(1) - 0\right] + 4\left[sY - 1\right] + 3Y = \frac{1}{s+2}.

Collect terms:

(s2+4s+3)Ys4=1s+2.(s^2 + 4s + 3)Y - s - 4 = \frac{1}{s+2}. (s2+4s+3)Y=s+4+1s+2=(s+4)(s+2)+1s+2=s2+6s+9s+2=(s+3)2s+2.(s^2 + 4s + 3)Y = s + 4 + \frac{1}{s+2} = \frac{(s+4)(s+2) + 1}{s+2} = \frac{s^2 + 6s + 9}{s+2} = \frac{(s+3)^2}{s+2}.

Since s2+4s+3=(s+1)(s+3)s^2 + 4s + 3 = (s+1)(s+3),

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

Partial fractions.

s+3(s+1)(s+2)=As+1+Bs+2.\frac{s+3}{(s+1)(s+2)} = \frac{A}{s+1} + \frac{B}{s+2}.

Multiply out: s+3=A(s+2)+B(s+1)s+3 = A(s+2) + B(s+1).

  • s=1s=-1: 1+3=A(1)A=2.-1+3 = A(1) \Rightarrow A = 2.
  • s=2s=-2: 2+3=B(1)B=1.-2+3 = B(-1) \Rightarrow B = -1.

So

Y=2s+11s+2.Y = \frac{2}{s+1} - \frac{1}{s+2}.

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

y(t)=2ete2t.y(t) = 2e^{-t} - e^{-2t}.

Verify initial conditions. y(0)=21=1y(0) = 2 - 1 = 1 ✓. y(t)=2et+2e2ty'(t) = -2e^{-t} + 2e^{-2t}, so y(0)=2+2=0y'(0) = -2 + 2 = 0 ✓.

Result.

y(t)=2ete2t\boxed{y(t) = 2e^{-t} - e^{-2t}}
laplace-transforminverse-laplacedifferential-equation
4long8 marks

State Cauchy's residue theorem. Hence evaluate

Cz2+1(z1)(z3)dz,\oint_C \frac{z^2 + 1}{(z-1)(z-3)}\,dz,

where CC is the circle z=2|z| = 2 described counterclockwise.

Cauchy's residue theorem. If f(z)f(z) is analytic inside and on a simple closed contour CC except for a finite number of isolated singularities 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).

Locate singularities. f(z)=z2+1(z1)(z3)f(z) = \dfrac{z^2+1}{(z-1)(z-3)} has simple poles at z=1z=1 and z=3z=3.

The contour is z=2|z|=2 (radius 2 about the origin):

  • z=1z=1: 1=1<2|1| = 1 < 2inside CC.
  • z=3z=3: 3=3>2|3| = 3 > 2outside CC.

Only z=1z=1 contributes.

Residue at the simple pole z=1z=1.

Resz=1f=limz1(z1)z2+1(z1)(z3)=z2+1z3z=1=1+113=22=1.\operatorname{Res}_{z=1} f = \lim_{z\to 1} (z-1)\,\frac{z^2+1}{(z-1)(z-3)} = \frac{z^2+1}{z-3}\bigg|_{z=1} = \frac{1+1}{1-3} = \frac{2}{-2} = -1.

Apply the theorem.

Cf(z)dz=2πi(1)=2πi.\oint_C f(z)\,dz = 2\pi i \cdot (-1) = -2\pi i.

Result.

z=2z2+1(z1)(z3)dz=2πi\boxed{\oint_{|z|=2} \frac{z^2+1}{(z-1)(z-3)}\,dz = -2\pi i}
complex-analysiscauchy-residue-theoremcontour-integral
5long8 marks

A tightly stretched string of length L=πL = \pi has its ends fixed at x=0x=0 and x=πx=\pi. It is released from rest with initial displacement u(x,0)=3sinxsin4xu(x,0) = 3\sin x - \sin 4x. Using the method of separation of variables, solve the one-dimensional wave equation

2ut2=c22ux2\frac{\partial^2 u}{\partial t^2} = c^2\,\frac{\partial^2 u}{\partial x^2}

subject to u(0,t)=u(π,t)=0u(0,t)=u(\pi,t)=0 and ut(x,0)=0u_t(x,0)=0, and write the explicit solution.

Separation of variables. Seek u(x,t)=X(x)T(t)u(x,t) = X(x)\,T(t). Substituting into the wave equation:

XT=c2XT    Tc2T=XX=λ  (const).X T'' = c^2 X'' T \;\Rightarrow\; \frac{T''}{c^2 T} = \frac{X''}{X} = -\lambda \;(\text{const}).

This gives two ODEs:

X+λX=0,T+λc2T=0.X'' + \lambda X = 0,\qquad T'' + \lambda c^2 T = 0.

Spatial problem and boundary conditions. u(0,t)=0X(0)=0u(0,t)=0 \Rightarrow X(0)=0; u(π,t)=0X(π)=0u(\pi,t)=0 \Rightarrow X(\pi)=0. For nontrivial solutions take λ=n2\lambda = n^2 (n=1,2,n=1,2,\dots):

Xn(x)=sin(nx),n=1,2,3,X_n(x) = \sin(nx),\qquad n=1,2,3,\dots

(the eigenvalues are λn=n2\lambda_n = n^2 because L=πL=\pi, so X(π)=sin(nπ)=0X(\pi)=\sin(n\pi)=0).

Time problem. T+n2c2T=0T'' + n^2 c^2 T = 0 gives

Tn(t)=ancos(nct)+bnsin(nct).T_n(t) = a_n\cos(nct) + b_n\sin(nct).

Apply the zero-initial-velocity condition ut(x,0)=0u_t(x,0)=0: this forces bn=0b_n = 0 for all nn (since Tn(0)=ncbn=0T_n'(0) = nc\,b_n = 0). 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)=3sinxsin4x.u(x,0) = \sum_{n=1}^{\infty} a_n \sin(nx) = 3\sin x - \sin 4x.

Matching coefficients term by term:

a1=3,a4=1,an=0 (n1,4).a_1 = 3,\qquad a_4 = -1,\qquad a_n = 0 \ (n \ne 1,4).

No Fourier integral is needed because the initial shape is already a finite sine series.

Explicit solution.

u(x,t)=3cos(ct)sinxcos(4ct)sin4x\boxed{u(x,t) = 3\cos(ct)\,\sin x - \cos(4ct)\,\sin 4x}

This satisfies the PDE, both fixed-end conditions, and the rest condition ut(x,0)=0u_t(x,0)=0.

partial-differential-equationwave-equationseparation-of-variables
B

Section B: Short Answer Questions

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6 questions
6short7 marks

Evaluate the double integral by changing to polar coordinates:

0204x2(x2+y2)dydx.\int_0^2 \int_0^{\sqrt{4-x^2}} \left(x^2 + y^2\right)\,dy\,dx.

Identify the region. For 0x20\le x\le 2 and 0y4x20\le y\le \sqrt{4-x^2}, the upper bound is the circle x2+y2=4x^2+y^2=4. With both x0x\ge 0 and y0y\ge 0, the region RR is the quarter disk of radius 22 in the first quadrant.

Polar substitution. Let x=rcosθ, y=rsinθx = r\cos\theta,\ y = r\sin\theta, so x2+y2=r2x^2+y^2 = r^2 and dA=rdrdθdA = r\,dr\,d\theta. The region becomes

0r2,0θπ2.0 \le r \le 2,\qquad 0 \le \theta \le \frac{\pi}{2}.

Transform the integral.

R(x2+y2)dA=0π/202r2rdrdθ=0π/202r3drdθ.\iint_R (x^2+y^2)\,dA = \int_0^{\pi/2}\int_0^2 r^2 \cdot r\,dr\,d\theta = \int_0^{\pi/2}\int_0^2 r^3\,dr\,d\theta.

Inner integral.

02r3dr=r4402=164=4.\int_0^2 r^3\,dr = \frac{r^4}{4}\Big|_0^2 = \frac{16}{4} = 4.

Outer integral.

0π/24dθ=4π2=2π.\int_0^{\pi/2} 4\,d\theta = 4\cdot\frac{\pi}{2} = 2\pi.

Result.

0204x2(x2+y2)dydx=2π6.2832\boxed{\int_0^2 \int_0^{\sqrt{4-x^2}} (x^2+y^2)\,dy\,dx = 2\pi \approx 6.2832}
multiple-integralpolar-coordinatesdouble-integral
7short7 marks

Given the scalar field ϕ=x2y+y2z+z2x\phi = x^2 y + y^2 z + z^2 x, find:

(a) ϕ\nabla\phi at the point P(1,2,1)P(1, 2, -1);

(b) 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) the maximum rate of change of ϕ\phi at PP and the direction in which it occurs.

(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) = \left(2xy + z^2,\; x^2 + 2yz,\; y^2 + 2zx\right).

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

  • ϕx=2(1)(2)+(1)2=4+1=5.\phi_x = 2(1)(2) + (-1)^2 = 4 + 1 = 5.
  • ϕy=(1)2+2(2)(1)=14=3.\phi_y = (1)^2 + 2(2)(-1) = 1 - 4 = -3.
  • ϕz=(2)2+2(1)(1)=42=2.\phi_z = (2)^2 + 2(-1)(1) = 4 - 2 = 2.
ϕP=5i3j+2k.\nabla\phi\big|_P = 5\mathbf{i} - 3\mathbf{j} + 2\mathbf{k}.

(b) Directional derivative. Unit vector along a=2ij+2k\mathbf{a} = 2\mathbf{i} - \mathbf{j} + 2\mathbf{k}:

a=22+(1)2+22=9=3,a^=13(2,1,2).|\mathbf{a}| = \sqrt{2^2 + (-1)^2 + 2^2} = \sqrt{9} = 3,\qquad \hat{\mathbf{a}} = \tfrac{1}{3}(2, -1, 2).

Then

Da^ϕ=ϕa^=13[(5)(2)+(3)(1)+(2)(2)]=13(10+3+4)=173.D_{\hat{\mathbf{a}}}\phi = \nabla\phi\cdot\hat{\mathbf{a}} = \frac{1}{3}\big[(5)(2) + (-3)(-1) + (2)(2)\big] = \frac{1}{3}(10 + 3 + 4) = \frac{17}{3}. Da^ϕ=1735.667.D_{\hat{\mathbf{a}}}\phi = \frac{17}{3} \approx 5.667.

(c) Maximum rate of change. This equals ϕ|\nabla\phi| and occurs in the direction of ϕ\nabla\phi:

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

in the direction 138(5i3j+2k)\dfrac{1}{\sqrt{38}}(5\mathbf{i} - 3\mathbf{j} + 2\mathbf{k}).

Results.

ϕP=5i3j+2k,Da^ϕ=173,ϕP=38\boxed{\nabla\phi|_P = 5\mathbf{i} - 3\mathbf{j} + 2\mathbf{k},\quad D_{\hat{\mathbf{a}}}\phi = \tfrac{17}{3},\quad |\nabla\phi|_P = \sqrt{38}}
vector-calculusgradientdirectional-derivative
8short7 marks

(a) Find the Laplace transform of f(t)=te3tcos2tf(t) = t\,e^{-3t}\cos 2t.

(b) Find the inverse Laplace transform of 2s+5s2+4s+13\dfrac{2s + 5}{s^2 + 4s + 13}.

(a) Laplace transform of te3tcos2tt\,e^{-3t}\cos 2t.

Start from L{cos2t}=ss2+4\mathcal{L}\{\cos 2t\} = \dfrac{s}{s^2 + 4}.

Apply the multiplication-by-tt rule L{tg(t)}=ddsL{g(t)}\mathcal{L}\{t\,g(t)\} = -\dfrac{d}{ds}\mathcal{L}\{g(t)\} to g(t)=cos2tg(t)=\cos 2t:

L{tcos2t}=dds ⁣(ss2+4)=(s2+4)(1)s(2s)(s2+4)2=4s2(s2+4)2=s24(s2+4)2.\mathcal{L}\{t\cos 2t\} = -\frac{d}{ds}\!\left(\frac{s}{s^2+4}\right) = -\frac{(s^2+4)(1) - s(2s)}{(s^2+4)^2} = -\frac{4 - s^2}{(s^2+4)^2} = \frac{s^2 - 4}{(s^2+4)^2}.

Now apply the first shifting theorem L{e3th(t)}=H(s+3)\mathcal{L}\{e^{-3t}h(t)\} = H(s+3) with h(t)=tcos2th(t)=t\cos 2t, i.e. replace ss by s+3s+3:

L{te3tcos2t}=(s+3)24[(s+3)2+4]2.\mathcal{L}\{t e^{-3t}\cos 2t\} = \frac{(s+3)^2 - 4}{\big[(s+3)^2 + 4\big]^2}.

Simplify (s+3)24=s2+6s+5(s+3)^2 - 4 = s^2 + 6s + 5 and (s+3)2+4=s2+6s+13(s+3)^2 + 4 = s^2 + 6s + 13:

L{te3tcos2t}=s2+6s+5(s2+6s+13)2\boxed{\mathcal{L}\{t e^{-3t}\cos 2t\} = \frac{s^2 + 6s + 5}{\left(s^2 + 6s + 13\right)^2}}

(b) Inverse transform of 2s+5s2+4s+13\dfrac{2s+5}{s^2+4s+13}.

Complete the square in the denominator: s2+4s+13=(s+2)2+9s^2 + 4s + 13 = (s+2)^2 + 9, where 9=329 = 3^2.

Write the numerator in terms of (s+2)(s+2):

2s+5=2(s+2)+1.2s + 5 = 2(s+2) + 1.

So

2s+5(s+2)2+9=2s+2(s+2)2+32+133(s+2)2+32.\frac{2s+5}{(s+2)^2 + 9} = 2\cdot\frac{s+2}{(s+2)^2 + 3^2} + \frac{1}{3}\cdot\frac{3}{(s+2)^2 + 3^2}.

Using L1 ⁣{s+a(s+a)2+b2}=eatcosbt\mathcal{L}^{-1}\!\left\{\dfrac{s+a}{(s+a)^2+b^2}\right\} = e^{-at}\cos bt and L1 ⁣{b(s+a)2+b2}=eatsinbt\mathcal{L}^{-1}\!\left\{\dfrac{b}{(s+a)^2+b^2}\right\} = e^{-at}\sin bt with a=2, b=3a=2,\ b=3:

L1 ⁣{2s+5s2+4s+13}=e2t(2cos3t+13sin3t)\boxed{\mathcal{L}^{-1}\!\left\{\frac{2s+5}{s^2+4s+13}\right\} = e^{-2t}\left(2\cos 3t + \tfrac{1}{3}\sin 3t\right)}
laplace-transformsecond-shiftingunit-step-function
9short7 marks

Find the Fourier cosine transform of

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

and hence, using the cosine inversion, deduce the value of the integral 0sinaωωdω\displaystyle \int_0^{\infty} \frac{\sin a\omega}{\omega}\,d\omega.

Fourier cosine transform. With the convention

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

and f(x)=1f(x)=1 on [0,a)[0,a), 00 otherwise:

Fc(ω)=2π0acos(ωx)dx=2π[sin(ωx)ω]0a=2πsinaωω.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 a\omega}{\omega}. Fc(ω)=2πsinaωω\boxed{F_c(\omega) = \sqrt{\frac{2}{\pi}}\,\frac{\sin a\omega}{\omega}}

Cosine inversion. The inversion formula is

f(x)=2π0Fc(ω)cos(ωx)dω=2π0sinaωωcos(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.

Evaluate at x=0x = 0. Here f(0)=1f(0) = 1 (interior point of the interval [0,a)[0,a)), so

1=2π0sinaωωdω.1 = \frac{2}{\pi}\int_0^{\infty} \frac{\sin a\omega}{\omega}\,d\omega.

Solving,

0sinaωωdω=π2.\int_0^{\infty} \frac{\sin a\omega}{\omega}\,d\omega = \frac{\pi}{2}.

(For a>0a>0 this is the standard Dirichlet integral; the value is independent of aa, since substituting u=aωu=a\omega gives 0sinuudu\int_0^\infty \frac{\sin u}{u}\,du.)

Result.

0sinaωωdω=π2(a>0)\boxed{\int_0^{\infty} \frac{\sin a\omega}{\omega}\,d\omega = \frac{\pi}{2}\quad (a>0)}
fourier-transformfourier-integraleven-function
10short7 marks

Show that the function u(x,y)=x33xy2+2yu(x,y) = x^3 - 3xy^2 + 2y is harmonic. Find its harmonic conjugate v(x,y)v(x,y) and express the corresponding analytic function f(z)=u+ivf(z) = u + iv in terms of zz.

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

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

Then

uxx+uyy=6x+(6x)=0,u_{xx} + u_{yy} = 6x + (-6x) = 0,

so uu satisfies Laplace's equation and is harmonic.

Find the conjugate vv via Cauchy–Riemann equations ux=vyu_x = v_y and uy=vxu_y = -v_x.

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 unknown function of xx.

Differentiate with respect to xx: vx=6xy+g(x)v_x = 6xy + g'(x). The second CR equation requires vx=uy=(6xy+2)=6xy2v_x = -u_y = -(-6xy + 2) = 6xy - 2. Hence

6xy+g(x)=6xy2    g(x)=2    g(x)=2x+C.6xy + g'(x) = 6xy - 2 \;\Rightarrow\; g'(x) = -2 \;\Rightarrow\; g(x) = -2x + C.

Taking the constant C=0C=0:

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

Form the analytic function.

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

Group the cubic and linear parts. Note x33xy2+i(3x2yy3)=(x+iy)3=z3x^3 - 3xy^2 + i(3x^2 y - y^3) = (x+iy)^3 = z^3. The remaining terms: 2y2ix=2i(x+iy)=2iz2y - 2ix = -2i(x + iy) = -2iz. Therefore

f(z)=z32iz  (+iC).f(z) = z^3 - 2iz \;(+\,iC).

Result.

v(x,y)=3x2yy32x,f(z)=z32iz\boxed{v(x,y) = 3x^2 y - y^3 - 2x,\qquad f(z) = z^3 - 2iz}
complex-analysisanalytic-functioncauchy-riemann
11short5 marks

(a) Classify the second-order PDE   3uxx+2uxy+5uyy+ux=0  \;3u_{xx} + 2u_{xy} + 5u_{yy} + u_x = 0\; as elliptic, parabolic, or hyperbolic.

(b) Form the partial differential equation by eliminating the arbitrary function ff from z=f(x2y2)z = f(x^2 - y^2).

(a) Classification. For a second-order PDE

Auxx+Buxy+Cuyy+(lower-order)=0,A u_{xx} + B u_{xy} + C u_{yy} + (\text{lower-order}) = 0,

the type is determined by the discriminant B24ACB^2 - 4AC:

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

Here A=3, B=2, C=5A = 3,\ B = 2,\ C = 5:

B24AC=(2)24(3)(5)=460=56<0.B^2 - 4AC = (2)^2 - 4(3)(5) = 4 - 60 = -56 < 0.

Since the discriminant is negative, the equation is elliptic (everywhere, as the coefficients are constant).

(b) Eliminate ff from z=f(x2y2)z = f(x^2 - y^2).

Let w=x2y2w = x^2 - y^2, so z=f(w)z = f(w). Differentiate:

p=zx=f(w)wx=f(w)(2x),p = \frac{\partial z}{\partial x} = f'(w)\cdot\frac{\partial w}{\partial x} = f'(w)\cdot(2x), q=zy=f(w)wy=f(w)(2y).q = \frac{\partial z}{\partial y} = f'(w)\cdot\frac{\partial w}{\partial y} = f'(w)\cdot(-2y).

Divide to eliminate the unknown f(w)f'(w) (assuming it is nonzero):

pq=2x2y=xy.\frac{p}{q} = \frac{2x}{-2y} = -\frac{x}{y}.

Cross-multiplying:

py=qx    yp+xq=0.p\,y = -q\,x \;\Rightarrow\; y\,p + x\,q = 0.

Result.

(a) Elliptic (B24AC=56<0);(b) yzx+xzy=0\boxed{(a)\ \text{Elliptic}\ (B^2-4AC=-56<0);\qquad (b)\ y\,\frac{\partial z}{\partial x} + x\,\frac{\partial z}{\partial y} = 0}
partial-differential-equationheat-equationclassification

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