← 2016 Paper 2

UPSC 2016 Maths Optional Paper 2 Q5b — Step-by-Step Solution

10 marks · Section B

Vortex motion; circulation · Mechanics & Fluid Dynamics · asked 6× in 14 yrs · Read the full method →

Question

Does a fluid with velocity q⃗=[z−2xr, 2y−3z−2yr, x−3y−2zr]\vec q=\left[z-\dfrac{2x}{r},\ 2y-3z-\dfrac{2y}{r},\ x-3y-\dfrac{2z}{r}\right] possess vorticity, where q⃗(u,v,w)\vec q(u,v,w) is the velocity in the Cartesian frame, r⃗=(x,y,z)\vec r=(x,y,z) and r2=x2+y2+z2r^2=x^2+y^2+z^2? What is the circulation in the circle x2+y2=9, z=0x^2+y^2=9,\ z=0?

Technique

Split into polynomial + radial parts; radial part is ∇(2r)\nabla(2r) hence curl-free; compute ∇×q⃗1\nabla\times\vec q_1 directly (all components cancel); circulation via Stokes = flux of the (zero) vorticity, cross-checked by a direct line integral.

Solution

Setup. The vorticity is ω⃗=∇×q⃗\vec\omega=\nabla\times\vec q. The field splits as a polynomial part plus a radial part:

q⃗=(z, 2y−3z, x−3y)⏟q⃗1 − 2r(x,y,z)⏟= 2r⃗/r.\vec q=\underbrace{(z,\ 2y-3z,\ x-3y)}_{\vec q_1}\ -\ \underbrace{\frac{2}{r}(x,y,z)}_{=\,2\vec r/r}.

Note 2r⃗r=∇(2r)\dfrac{2\vec r}{r}=\nabla(2r) since ∇r=r⃗/r\nabla r=\vec r/r; any gradient is curl-free. So the radial part contributes nothing to ω⃗\vec\omega, and we only need the curl of q⃗1\vec q_1.

Step 1 — Vorticity of the radial part

2r⃗r=2 ∇r=∇(2r) ⇒ ∇×(2r⃗r)=∇×∇(2r)=0⃗.\frac{2\vec r}{r}=2\,\nabla r=\nabla(2r)\ \Rightarrow\ \nabla\times\Big(\frac{2\vec r}{r}\Big)=\nabla\times\nabla(2r)=\vec 0.

Step 2 — Vorticity of the polynomial part

With u1=z, v1=2y−3z, w1=x−3yu_1=z,\ v_1=2y-3z,\ w_1=x-3y:

∇×q⃗1=(∂w1∂y−∂v1∂z, ∂u1∂z−∂w1∂x, ∂v1∂x−∂u1∂y).\nabla\times\vec q_1=\left(\frac{\partial w_1}{\partial y}-\frac{\partial v_1}{\partial z},\ \frac{\partial u_1}{\partial z}-\frac{\partial w_1}{\partial x},\ \frac{\partial v_1}{\partial x}-\frac{\partial u_1}{\partial y}\right). ∂w1∂y−∂v1∂z=(−3)−(−3)=0,\frac{\partial w_1}{\partial y}-\frac{\partial v_1}{\partial z}=(-3)-(-3)=0, ∂u1∂z−∂w1∂x=1−1=0,\frac{\partial u_1}{\partial z}-\frac{\partial w_1}{\partial x}=1-1=0, ∂v1∂x−∂u1∂y=0−0=0.\frac{\partial v_1}{\partial x}-\frac{\partial u_1}{\partial y}=0-0=0.

So ∇×q⃗1=0⃗\nabla\times\vec q_1=\vec 0 as well.

Step 3 — Conclusion on vorticity

  ω⃗=∇×q⃗=0⃗⇒the fluid has no vorticity (flow is irrotational).  \boxed{\;\vec\omega=\nabla\times\vec q=\vec 0\quad\Rightarrow\quad\text{the fluid has \textbf{no vorticity} (flow is irrotational).}\;}

(The polynomial part is antisymmetric in just the right way — each off-diagonal derivative cancels its partner — and the radial part is a pure gradient.)

Step 4 — Circulation around the circle

By Stokes’ theorem, the circulation around the circle C: x2+y2=9, z=0C:\ x^2+y^2=9,\ z=0 (a disc DD in the plane z=0z=0, normal k^\hat k) is

Γ=∮Cq⃗⋅dr⃗=∬D(∇×q⃗)⋅k^ dS=∬D0 dS=0.\Gamma=\oint_C\vec q\cdot d\vec r=\iint_D(\nabla\times\vec q)\cdot\hat k\,dS=\iint_D 0\,dS=0.

Answer

  Γ=0.  \boxed{\;\Gamma=0.\;}
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