← 2022 Paper 2

UPSC 2022 Maths Optional Paper 2 Q5e — Step-by-Step Solution

10 marks · Section B

Potential flow · Mechanics & Fluid Dynamics · asked 10× in 13 yrs · Read the full method →

Question

Velocity components in spherical polar (r,θ,ψ)(r,\theta,\psi): vr=2Mr3cosθv_r=2Mr^{-3}\cos\theta, vθ=Mr2sinθv_\theta=Mr^{-2}\sin\theta, vψ=0v_\psi=0. Show velocity is of potential kind. Find velocity potential and streamlines.

Technique

Standard 3D doublet flow; verify irrotationality, recover potential by ϕ=v\nabla\phi=\vec v, recover stream function by vr=(1/(r2sinθ))θψv_r=(1/(r^2\sin\theta))\partial_\theta\psi.

Solution

Wait — re-read: the velocity is (2Mr3cosθ,Mr2sinθ,0)(2Mr^{-3}\cos\theta, Mr^{-2}\sin\theta, 0). The r3r^{-3} and r2r^{-2} factors suggest dipole-like flow.

Step 1 — Test for potential flow

Velocity is of potential kind iff ×v=0\nabla\times\vec v=0 (irrotational).

In spherical: ×v\nabla\times\vec v has ψ\psi-component 1r ⁣[(rvθ)rvrθ]\dfrac{1}{r}\!\left[\dfrac{\partial(rv_\theta)}{\partial r}-\dfrac{\partial v_r}{\partial\theta}\right].

rvθ=rMr2sinθ=Mr1sinθrv_\theta=r\cdot Mr^{-2}\sin\theta=Mr^{-1}\sin\theta.

(rvθ)/r=Mr2sinθ\partial(rv_\theta)/\partial r=-Mr^{-2}\sin\theta.

vr/θ=2Mr3(sinθ)=2Mr3sinθ\partial v_r/\partial\theta=2Mr^{-3}(-\sin\theta)=-2Mr^{-3}\sin\theta.

Hmm wait — the formula for curl in spherical (assuming axisymmetric, no ψ\psi dependence):

(×v)ψ=1r ⁣[(rvθ)rvrθ](\nabla\times\vec v)_\psi=\dfrac{1}{r}\!\left[\dfrac{\partial(rv_\theta)}{\partial r}-\dfrac{\partial v_r}{\partial\theta}\right]

Hmm — let me look this up. The full curl in spherical (r,θ,ϕ)(r,\theta,\phi):

(×v)ϕ=1r ⁣[(rvθ)rvrθ](\nabla\times\vec v)_\phi=\dfrac{1}{r}\!\left[\dfrac{\partial(rv_\theta)}{\partial r}-\dfrac{\partial v_r}{\partial\theta}\right].

Substitute: (rvθ)r=(Mr1sinθ)r=Mr2sinθ\dfrac{\partial(rv_\theta)}{\partial r}=\dfrac{\partial(Mr^{-1}\sin\theta)}{\partial r}=-Mr^{-2}\sin\theta.

vrθ=(2Mr3cosθ)θ=2Mr3sinθ\dfrac{\partial v_r}{\partial\theta}=\dfrac{\partial(2Mr^{-3}\cos\theta)}{\partial\theta}=-2Mr^{-3}\sin\theta.

(×v)ϕ=1r[Mr2sinθ(2Mr3sinθ)]=1r ⁣[Mr2+2Mr3]sinθ(\nabla\times\vec v)_\phi=\dfrac{1}{r}[-Mr^{-2}\sin\theta-(-2Mr^{-3}\sin\theta)]=\dfrac{1}{r}\!\left[-Mr^{-2}+2Mr^{-3}\right]\sin\theta.

For irrotational: need this =0=0. But Mr2+2Mr3-Mr^{-2}+2Mr^{-3} does not vanish identically; it depends on rr.

Hmm — likely a typo or misreading. Let me re-examine the problem.

Actually, re-reading the velocity components: vr=2Mr3cosθv_r=2Mr^{-3}\cos\theta, vθ=Mr3sinθv_\theta=Mr^{-3}\sin\theta (note r3r^{-3} not r2r^{-2}). Let me retry with vθ=Mr3sinθv_\theta=Mr^{-3}\sin\theta.

Hmm but the question states vθ=Mr2sinθv_\theta=Mr^{-2}\sin\theta. Let me just check if this is the dipole formula.

Standard dipole flow. A 3D doublet of strength μ\mu aligned with zz-axis has velocity potential ϕ=μcosθ/r2\phi=-\mu\cos\theta/r^2. Then vr=ϕ/r=2μcosθ/r3v_r=\partial\phi/\partial r=2\mu\cos\theta/r^3 and vθ=(1/r)ϕ/θ=(1/r)(μsinθ/r2)=μsinθ/r3v_\theta=(1/r)\partial\phi/\partial\theta=(1/r)\cdot(\mu\sin\theta/r^2)=\mu\sin\theta/r^3.

So the standard dipole has vrr3v_r\sim r^{-3} and vθr3v_\theta\sim r^{-3}, both with the same factor.

The question’s vθ=Mr2sinθv_\theta=Mr^{-2}\sin\theta has a different exponent. Likely a typo; assuming vθ=Mr3sinθv_\theta=Mr^{-3}\sin\theta (matching dipole):

(rvθ)/r=(Mr2sinθ)/r=2Mr3sinθ\partial(rv_\theta)/\partial r=\partial(Mr^{-2}\sin\theta)/\partial r=-2Mr^{-3}\sin\theta.

vr/θ=2Mr3sinθ\partial v_r/\partial\theta=-2Mr^{-3}\sin\theta.

(×v)ϕ=1r ⁣[2Mr3sinθ(2Mr3sinθ)]=0(\nabla\times\vec v)_\phi=\dfrac{1}{r}\!\left[-2Mr^{-3}\sin\theta-(-2Mr^{-3}\sin\theta)\right]=0 ✓.

Assuming the corrected formula vθ=Mr3sinθv_\theta=Mr^{-3}\sin\theta, flow is irrotational.

Step 2 — Find velocity potential

vr=ϕ/r=2Mcosθ/r3v_r=\partial\phi/\partial r=2M\cos\theta/r^3.

Integrate w.r.t. rr: ϕ=Mcosθ/r2+g(θ)\phi=-M\cos\theta/r^2+g(\theta).

vθ=(1/r)ϕ/θ=(1/r)[Msinθ/r2+g(θ)]=Msinθ/r3+g(θ)/rv_\theta=(1/r)\partial\phi/\partial\theta=(1/r)\cdot[M\sin\theta/r^2+g'(\theta)]=M\sin\theta/r^3+g'(\theta)/r.

Match vθ=Msinθ/r3v_\theta=M\sin\theta/r^3: g(θ)/r=0g'(\theta)/r=0, so g(θ)=0g'(\theta)=0, g=g= const.

  ϕ(r,θ)=Mcosθr2.  \boxed{\;\phi(r,\theta)=-\dfrac{M\cos\theta}{r^2}.\;}

This is the classical 3D doublet (dipole) potential of strength MM aligned with the zz-axis.

Step 3 — Streamlines

For axisymmetric flow, the stream function ψ\psi satisfies vr=1r2sinθθψv_r=\dfrac{1}{r^2\sin\theta}\partial_\theta\psi, vθ=1rsinθrψv_\theta=-\dfrac{1}{r\sin\theta}\partial_r\psi.

From vr=2Mcosθ/r3v_r=2M\cos\theta/r^3: θψ=vrr2sinθ=2Mcosθsinθ/r\partial_\theta\psi=v_r\cdot r^2\sin\theta=2M\cos\theta\sin\theta/r.

Integrate w.r.t. θ\theta: ψ=Mcos2θ/r+h(r)\psi=-M\cos^2\theta/r+h(r)? Let me use 2sinθcosθ=sin2θ2\sin\theta\cos\theta=\sin 2\theta — then 2sinθcosθdθ=cos2θ/...\int 2\sin\theta\cos\theta\,d\theta=-\cos 2\theta/...

Actually sinθcosθdθ=sin2θ/2\int\sin\theta\cos\theta\,d\theta=\sin^2\theta/2 (since d(sin2θ)/dθ=2sinθcosθd(\sin^2\theta)/d\theta=2\sin\theta\cos\theta).

So ψ=Msin2θr+h(r)\psi=\dfrac{M\sin^2\theta}{r}+h(r).

Wait: θψ=2Mcosθsinθ/r=(M/r)sin2θ=(M/r)2sinθcosθ\partial_\theta\psi=2M\cos\theta\sin\theta/r=(M/r)\sin 2\theta=(M/r)\cdot 2\sin\theta\cos\theta. Integrating w.r.t. θ\theta: (M/r)sin2θ+h(r)(M/r)\cdot\sin^2\theta+h(r) (since d(sin2θ)/dθ=2sinθcosθd(\sin^2\theta)/d\theta=2\sin\theta\cos\theta).

So ψ=Msin2θ/r+h(r)\psi=M\sin^2\theta/r+h(r).

Check vθ=(1/(rsinθ))rψ=(1/(rsinθ))[Msin2θ/r2+h(r)]v_\theta=-(1/(r\sin\theta))\partial_r\psi=-(1/(r\sin\theta))[-M\sin^2\theta/r^2+h'(r)].

=Msinθr3h(r)rsinθ=\dfrac{M\sin\theta}{r^3}-\dfrac{h'(r)}{r\sin\theta}.

Match vθ=Msinθ/r3v_\theta=M\sin\theta/r^3: h(r)/(rsinθ)=0h'(r)/(r\sin\theta)=0, so h(r)=0h'(r)=0, h=h= const.

Answer

  ψ=Msin2θr.  \boxed{\;\psi=\dfrac{M\sin^2\theta}{r}.\;}
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