← 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 14 yrs · Read the full method →

Question

Velocity components in spherical polar (r,θ,ψ)(r,\theta,\psi): vr=2Mr−3cos⁡θv_r=2Mr^{-3}\cos\theta, vθ=Mr−2sin⁡θv_\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=v⃗\nabla\phi=\vec v, recover stream function by vr=(1/(r2sin⁡θ))∂θψv_r=(1/(r^2\sin\theta))\partial_\theta\psi.

Solution

Wait — re-read: the velocity is (2Mr−3cos⁡θ,Mr−2sin⁡θ,0)(2Mr^{-3}\cos\theta, Mr^{-2}\sin\theta, 0). The r−3r^{-3} and r−2r^{-2} factors suggest dipole-like flow.

Step 1 — Test for potential flow

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

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

rvθ=r⋅Mr−2sin⁡θ=Mr−1sin⁡θrv_\theta=r\cdot Mr^{-2}\sin\theta=Mr^{-1}\sin\theta.

∂(rvθ)/∂r=−Mr−2sin⁡θ\partial(rv_\theta)/\partial r=-Mr^{-2}\sin\theta.

∂vr/∂θ=2Mr−3(−sin⁡θ)=−2Mr−3sin⁡θ\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):

(∇×v⃗)ψ=1r ⁣[∂(rvθ)∂r−∂vr∂θ](\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):

(∇×v⃗)ϕ=1r ⁣[∂(rvθ)∂r−∂vr∂θ](\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=∂(Mr−1sin⁡θ)∂r=−Mr−2sin⁡θ\dfrac{\partial(rv_\theta)}{\partial r}=\dfrac{\partial(Mr^{-1}\sin\theta)}{\partial r}=-Mr^{-2}\sin\theta.

∂vr∂θ=∂(2Mr−3cos⁡θ)∂θ=−2Mr−3sin⁡θ\dfrac{\partial v_r}{\partial\theta}=\dfrac{\partial(2Mr^{-3}\cos\theta)}{\partial\theta}=-2Mr^{-3}\sin\theta.

(∇×v⃗)ϕ=1r[−Mr−2sin⁡θ−(−2Mr−3sin⁡θ)]=1r ⁣[−Mr−2+2Mr−3]sin⁡θ(\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 −Mr−2+2Mr−3-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=2Mr−3cos⁡θv_r=2Mr^{-3}\cos\theta, vθ=Mr−3sin⁡θv_\theta=Mr^{-3}\sin\theta (note r−3r^{-3} not r−2r^{-2}). Let me retry with vθ=Mr−3sin⁡θv_\theta=Mr^{-3}\sin\theta.

Hmm but the question states vθ=Mr−2sin⁡θv_\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=−μcos⁡θ/r2\phi=-\mu\cos\theta/r^2. Then vr=∂ϕ/∂r=2μcos⁡θ/r3v_r=\partial\phi/\partial r=2\mu\cos\theta/r^3 and vθ=(1/r)∂ϕ/∂θ=(1/r)⋅(μsin⁡θ/r2)=μsin⁡θ/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 vr∼r−3v_r\sim r^{-3} and vθ∼r−3v_\theta\sim r^{-3}, both with the same factor.

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

∂(rvθ)/∂r=∂(Mr−2sin⁡θ)/∂r=−2Mr−3sin⁡θ\partial(rv_\theta)/\partial r=\partial(Mr^{-2}\sin\theta)/\partial r=-2Mr^{-3}\sin\theta.

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

(∇×v⃗)ϕ=1r ⁣[−2Mr−3sin⁡θ−(−2Mr−3sin⁡θ)]=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=Mr−3sin⁡θv_\theta=Mr^{-3}\sin\theta, flow is irrotational.

Step 2 — Find velocity potential

vr=∂ϕ/∂r=2Mcos⁡θ/r3v_r=\partial\phi/\partial r=2M\cos\theta/r^3.

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

vθ=(1/r)∂ϕ/∂θ=(1/r)⋅[Msin⁡θ/r2+g′(θ)]=Msin⁡θ/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=Msin⁡θ/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)=−Mcos⁡θr2.  \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=1r2sin⁡θ∂θψv_r=\dfrac{1}{r^2\sin\theta}\partial_\theta\psi, vθ=−1rsin⁡θ∂rψv_\theta=-\dfrac{1}{r\sin\theta}\partial_r\psi.

From vr=2Mcos⁡θ/r3v_r=2M\cos\theta/r^3: ∂θψ=vr⋅r2sin⁡θ=2Mcos⁡θsin⁡θ/r\partial_\theta\psi=v_r\cdot r^2\sin\theta=2M\cos\theta\sin\theta/r.

Integrate w.r.t. θ\theta: ψ=−Mcos⁡2θ/r+h(r)\psi=-M\cos^2\theta/r+h(r)? Let me use 2sin⁡θcos⁡θ=sin⁡2θ2\sin\theta\cos\theta=\sin 2\theta — then ∫2sin⁡θcos⁡θ dθ=−cos⁡2θ/...\int 2\sin\theta\cos\theta\,d\theta=-\cos 2\theta/...

Actually ∫sin⁡θcos⁡θ dθ=sin⁡2θ/2\int\sin\theta\cos\theta\,d\theta=\sin^2\theta/2 (since d(sin⁡2θ)/dθ=2sin⁡θcos⁡θd(\sin^2\theta)/d\theta=2\sin\theta\cos\theta).

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

Wait: ∂θψ=2Mcos⁡θsin⁡θ/r=(M/r)sin⁡2θ=(M/r)⋅2sin⁡θcos⁡θ\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)⋅sin⁡2θ+h(r)(M/r)\cdot\sin^2\theta+h(r) (since d(sin⁡2θ)/dθ=2sin⁡θcos⁡θd(\sin^2\theta)/d\theta=2\sin\theta\cos\theta).

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

Check vθ=−(1/(rsin⁡θ))∂rψ=−(1/(rsin⁡θ))[−Msin⁡2θ/r2+h′(r)]v_\theta=-(1/(r\sin\theta))\partial_r\psi=-(1/(r\sin\theta))[-M\sin^2\theta/r^2+h'(r)].

=Msin⁡θr3−h′(r)rsin⁡θ=\dfrac{M\sin\theta}{r^3}-\dfrac{h'(r)}{r\sin\theta}.

Match vθ=Msin⁡θ/r3v_\theta=M\sin\theta/r^3: h′(r)/(rsin⁡θ)=0h'(r)/(r\sin\theta)=0, so h′(r)=0h'(r)=0, h=h= const.

Answer

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