← 2015 Paper 2

UPSC 2015 Maths Optional Paper 2 Q5d — Step-by-Step Solution

10 marks · Section B

Sources, sinks, doublets · Mechanics & Fluid Dynamics · asked 9× in 14 yrs · Read the full method →

Question

Consider a uniform flow U0U_0 in the positive xx-direction. A cylinder of radius aa is located at the origin. Find the stream function and the velocity potential. Find also the stagnation points.

Technique

Standard “uniform flow + image doublet” complex potential; separate real and imaginary parts; impose ψ=0\psi=0 on cylinder surface (r=ar=a); stagnation points where ∇ϕ=0\nabla\phi=0.

Solution

Setup. 2D incompressible irrotational flow past a circular cylinder. Use polar coordinates (r,θ)(r,\theta) with origin at cylinder centre.

For uniform flow U0U_0 in the +x+x direction superposed with a doublet at the origin (so the cylinder surface r=ar=a is a streamline), the standard result is:

Step 1 — Complex potential

w(z)=U0 ⁣(z+a2z).w(z)=U_0\!\left(z+\dfrac{a^2}{z}\right).

(Uniform flow U0zU_0 z + doublet U0a2/zU_0 a^2/z.)

Step 2 — Velocity potential ϕ\phi and stream function ψ\psi

w=ϕ+iψw=\phi+i\psi with z=reiθz=re^{i\theta}:

U0 ⁣(reiθ+a2re−iθ)=U0 ⁣[(r+a2r)cos⁡θ+i(r−a2r)sin⁡θ].U_0\!\left(re^{i\theta}+\dfrac{a^2}{r}e^{-i\theta}\right)=U_0\!\left[\left(r+\dfrac{a^2}{r}\right)\cos\theta+i\left(r-\dfrac{a^2}{r}\right)\sin\theta\right].

So

  ϕ(r,θ)=U0 ⁣(r+a2r)cos⁡θ,ψ(r,θ)=U0 ⁣(r−a2r)sin⁡θ.  \boxed{\;\phi(r,\theta)=U_0\!\left(r+\dfrac{a^2}{r}\right)\cos\theta,\quad\psi(r,\theta)=U_0\!\left(r-\dfrac{a^2}{r}\right)\sin\theta.\;}

Step 3 — Verify cylinder is a streamline

At r=ar=a: ψ=U0(a−a)sin⁡θ=0\psi=U_0(a-a)\sin\theta=0. So the cylinder surface r=ar=a is the streamline ψ=0\psi=0 ✓.

Step 4 — Stagnation points

Velocity components:

vr=1r∂ψ∂θ=U0 ⁣(1−a2r2)cos⁡θ,v_r=\dfrac{1}{r}\dfrac{\partial\psi}{\partial\theta}=U_0\!\left(1-\dfrac{a^2}{r^2}\right)\cos\theta, vθ=−∂ψ∂r=−U0 ⁣(1+a2r2)sin⁡θ.v_\theta=-\dfrac{\partial\psi}{\partial r}=-U_0\!\left(1+\dfrac{a^2}{r^2}\right)\sin\theta.

Stagnation: vr=vθ=0v_r=v_\theta=0.

vr=0⇒v_r=0\Rightarrow either r=ar=a or cos⁡θ=0\cos\theta=0 (i.e. θ=±π/2\theta=\pm\pi/2). vθ=0⇒sin⁡θ=0v_\theta=0\Rightarrow \sin\theta=0 (i.e. θ=0\theta=0 or π\pi); 1+a2/r2>01+a^2/r^2>0 always.

Combining: vθ=0v_\theta=0 requires sin⁡θ=0\sin\theta=0, then vr=U0(1−a2/r2)cos⁡θ=0v_r=U_0(1-a^2/r^2)\cos\theta=0 requires r=ar=a (since cos⁡θ=±1≠0\cos\theta=\pm 1\ne 0).

Stagnation points: r=ar=a, θ=0\theta=0 or π\pi — i.e. (a,0)(a,0) (front of cylinder) and (−a,0)(-a,0) (rear).

In Cartesian: (a,0)(a,0) and (−a,0)(-a,0).

Answer

  Stagnation points: (±a,0).  \boxed{\;\text{Stagnation points: }(\pm a,0).\;}
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