Detailed Solutions Mathematics-II A-35/C-35/T-35 December 2004
1. (a) D ![]()

which is circle in (u,v) plane with centre (3,2).
(c) C Let ![]()

z=0 is an essential singularity.
(d) B
Let f = x3-xyz-1,
The normal to surface at point (1,1,1) is

(e) A
Using
Green’s Lemma.
(f) B The given differential equation is

It is elliptic if B2-4AC<0 i.e. x2<y2
(g) A V(3x+4)=E((3x+4)2) – (E(3x+4))2
= 9E(x2)+24E(x)+16-(3E(x)+4)2 = 9E(x2)-9(E(x))2= 9V(x)=9
(h) B As P(X
< 0) = P(X > 2).
0, 2 are symmetrically placed around
.
![]()
=
.
2. (a) It is given that 3u+2v=y2-x2+16xy, thus differentiating partially w.r.t.x and y
or ![]()
Solving, we get ux=2x+4y and vx=-4x+2y
Thus f ’(z)= ux+ ivx=2x+4y+i(2y-4x)
By Milne’s Thomson method, putting x=z and y=0, we get
f’(z)=2(1-2i)z Thus f(z) = (1-2i)z2+c.
(b) Let w=u+iv, and

Since w is an analytic function, thus
=
and ![]()
Thus
. Hence
cut orthogonally.
3. (a) Let w = 1/z, then z = 1/w. Thus
![]()
Since y ≤ 1/2,
thus u2+ v2+2v ≥ 0 or u2+ (v+1)2 ≥
1 i.e. ![]()
The boundary of this region is the outside of the circle with centre at(0,-1) and
radius 1,The region y ≥ 1/4 is transformed to
,

The boundary of this region is the outside of the circle with centre at (0,-2i) and
radius 2. Hence,
the infinite strip
maps into inside of the circle
and outside of
the circle
.
See the shaded region in the figure.
3(b) Since, w1=0, w2=1, w3=∞, and z1 = i, z2=-1, z3=1.
The bilinear transformation is given by

. Solving for z
gives
![]()

Thus interior of
the circle
,
in z plane is mapped onto the Imw > 0.
4. (a) It is given that

![]()
\ Given vector is irrotational. Thus it can
be expressed as
where f is scalar function.
,
,![]()
Integrating w.r.t. x, y, z we get

Since these three must be equal
+c
(b) ![]()
A vector normal to the surface xln(z) - y2 + 4 = 0 is given by
which at point
(-1,2,1) becomes
. The required directional
derivative is the component of
along
,
.
5. (a) ![]()
At C: x2 + y2
= a2, z=0, thus
.
Work = ![]()
where R is the region bounded by circle x2 + y2 = a2. Let x=rcosθ, y=rsinθ, then
dxdy=rdrdθ , where r changes from 0 to a and θ changes from 0 to 2π.
Thus work =
.
(b)


\ Given vector represents a conservative
field. Thus it can be expressed as
where f is scalar function.
,
,![]()
Integrating w.r.t. x, y, z we get

Since these three must be equal
![]()
Also, 
6. (i) Let the equation for conduction of heat be
![]()
Prior to temperature change at end B, when t = 0, the heat flow was independent of time (steady state condition), when u depends only on x i.e.
![]()
Since u = 100 for x = 0 and x = L
\ b = 100 and a = 0.
Thus initial condition is expressed as
![]()
The boundary conditions are

(ii) Assuming
product solution u(x,t) = X(x). T(t) and substituting in equation (1), we get ![]()
Case I :
If
(4)
gives![]()
Solving we have the solution
This solution is rejected as exponential term makes temperature u(x,t) increases without bounds as t → ∞.
Case II
: If
= 0. (4) gives
![]()
Integrating, we obtain X = (A X + B) and T = C.
Thus we can write
u(x,t) = (A1 X + B1), where A1 = AC and B1
=BC are arbitrary constant. Using boundary conditions (3), we get
is a solution
of heat equation.
Case III
: If
then
from (4) (as in case (I)) we conclude that
![]()
Since we already have a solution (5) satisfying boundary conditions (3) we can find A, B in (6) by satisfying the condition u(0,t) = 0 =u(l,t) which gives A = 0, B sinλl = 0 .
As B = 0 leads to
trivial solution we must have sinλl = 0 or
, n =1,2,….. Combining (5)
and (6), we have

as a general solution of (1).
Applying initial condition (2) to the general solution we must have
![]()
implies that
are the
coefficient in half range sine series expansion of

Putting
in (7) we get
required solution.
7(a) ![]()
If
then f(z) =
is analytic
within and on C. Thus
=0, by Cauchy Theorem if
.
If
the singularity
of f(z) =
lies within C and by Cauchy integral formula ![]()
Since
, ![]()
Since
is constant, then
.
7(b)
,
z=1, is apole of order 1 and z=-2 is a pole of order 2.
Expanding about z=1,
let z-1=t, i.e. z=t+1,
![]()

Since there is only one term in negative powers of (z-1), therefore z = 1,
is a pole of order 1. Residue at z = 1 is the coefficient of 1/t, which is 1/9.
.
Expanding about z=-2,
let z+2=t, i.e. z=t-2,
![]()
![]()
Since there are only two terms in negative powers of (z+2), therefore z = -2, is a pole of order 2. Residue is the coefficient of 1/t, which is 8/9.
.
8(a) Let the position vector of a point on C, in terms of arc length s be
. Then the tangent vector
to C is given by
and a normal vector
is given by
. Thus
,
since
is a directional
derivative of u in the direction of
. Now, using Green’s theorem, we
obtain




Also,
,
where S1, S2, S3, S4, S5 and S6 are the six faces of the cuboid.
On S1, ![]()
On S2 , 
On S3, ![]()
On S4, 
On S5, ![]()
On S6, 
Thus ![]()
Hence Gauss Divergence theorem is verified.
9(a) Let X be the number of engines that do not fail and let Sk denote the successful flight with k engine plane. Let 1-p=q,
P(S2)
= P(X ≥ 1) = 1-P(X=0)= 1-q2,![]()
P(S4) = P(X≥2) = 1-P(X=0)-P(X=1)= 1-4q3+3q4.
For P(S4) > P(S2), we have
1-4q3+3q4 > 1- q2 or q2(1-q)(1-3q) > 0.
If 0<q<1/3, i.e. 2/3<p<1, the four engine plane is preferred.
9(b) Given
that ![]()
Expected
number of wires in a sample of 1000 with this specification
= 1000(0.6826)=682.6=683 approximately.
![]()
Hence, expected number among 1000 wires that cross the upper specification = 1000(0.1587)=158.7=159 approximately.
10(i) P(400-C≤ L≤ 400+C)=11/16

Since
C≠
as it is either >1 or <1. Thus C=1/2.
(ii) E(L) = E(400+X) = 400+E(X)

Thus E(L) = 400.
V(L) = V(400+X) = V(X) = E(X2), as E(X) = 0
![]()
Thus E(L) = 400, V(L) = 0.2. Therefore,
E(2L+5) = 2E(L) + 5=805
V(2L+5) = 4V(L) = 0.8.
![]()
Since integrand is an even function, thus
![]()
Consider the
contour integral
and C is the path from –R to R
along the real axis and from R to –R along CR . Now f(z) is analytic
in upper half of the plane except at z=ai, which is pole of order 1.

Residue of f(z) at

by Residue
theorem.
Now,
. Therefore, by
Jordan’s Lemma

![]()
Equating imaginary part, we get
![]()

=

