🧮 Brain Teaser

The Conformal Map That Doubles Its Angle

Let f:C∖{0}→Cf : \mathbb{C} \setminus \{0\} \to \mathbb{C} be defined by f(z)=z+1z.f(z) = z + \frac{1}{z}.

(a) Show that ff maps the upper unit semicircle {eiθ:0<θ<π}\{e^{i\theta} : 0 < \theta < \pi\} to the interval (−2,2)(-2, 2) on the real axis.

(b) Show that ff maps the upper half of any circle ∣z∣=r|z| = r with r≠1r \neq 1 to an ellipse, and identify its semi-axes.

(c) Conclude: what does ff do to the family of concentric circles ∣z∣=r>0|z| = r > 0 and the family of rays arg⁡(z)=θ\arg(z) = \theta? Where do you see this map "in the wild"?

Joukowski mapconformal mappingelliptic coordinatescomplex analysisaerodynamics

Answer: The Conformal Map That Doubles Its Angle

Key Idea / Intuition

The Joukowski map f(z)=z+1/zf(z) = z + 1/z is one of the most celebrated maps in classical complex analysis and aerodynamics. The core insight is that writing z=reiθz = r e^{i\theta} separates the map into a real part depending on cos⁡θ\cos\theta and an imaginary part depending on sin⁡θ\sin\theta, weighted by r+1/rr + 1/r and r−1/rr - 1/r respectively. When r=1r = 1 the imaginary part vanishes (the circle collapses to a segment), and for r≠1r \neq 1 you get an ellipse whose axes are controlled by those two weights.


Formal Proof / Solution

Setup: polar decomposition

Write z=reiθz = r e^{i\theta}. Then

f(z)=reiθ+1re−iθ=(r+1r)cos⁡θ+i(r−1r)sin⁡θ.f(z) = re^{i\theta} + \frac{1}{r}e^{-i\theta} = \left(r + \frac{1}{r}\right)\cos\theta + i\left(r - \frac{1}{r}\right)\sin\theta.

So if we set u=Re⁡f(z)u = \operatorname{Re} f(z) and v=Im⁡f(z)v = \operatorname{Im} f(z):

u=(r+1r)cos⁡θ,v=(r−1r)sin⁡θ.u = \left(r + \frac{1}{r}\right)\cos\theta, \qquad v = \left(r - \frac{1}{r}\right)\sin\theta.


Part (a): Unit circle r=1r = 1

When r=1r = 1:

u=2cos⁡θ,v=0.u = 2\cos\theta, \qquad v = 0.

So f(eiθ)=2cos⁡θ∈Rf(e^{i\theta}) = 2\cos\theta \in \mathbb{R}. As θ\theta ranges over (0,π)(0, \pi), cos⁡θ\cos\theta ranges over (−1,1)(-1, 1), so ff maps the upper unit semicircle bijectively onto the open interval (−2,2)(-2, 2) on the real axis. ■\blacksquare

This is the key degeneration: the circle collapses to a segment because the imaginary coefficient r−1/r=0r - 1/r = 0.


Part (b): Circle of radius r≠1r \neq 1

For fixed r≠1r \neq 1, let

A=r+1r>0,B=∣r−1r∣>0.A = r + \frac{1}{r} > 0, \qquad B = \left|r - \frac{1}{r}\right| > 0.

Then u=Acos⁡θu = A\cos\theta, v=±Bsin⁡θv = \pm B\sin\theta (sign depending on whether r>1r > 1 or r<1r < 1). Eliminating θ\theta:

u2A2+v2B2=cos⁡2θ+sin⁡2θ=1.\frac{u^2}{A^2} + \frac{v^2}{B^2} = \cos^2\theta + \sin^2\theta = 1.

So the image is the ellipse with semi-major axis A=r+1/rA = r + 1/r (along the real axis) and semi-minor axis B=∣r−1/r∣B = |r - 1/r| (along the imaginary axis). ■\blacksquare

Check: As r→1r \to 1, B→0B \to 0 and the ellipse degenerates to the segment [−2,2][-2,2], consistent with part (a).


Part (c): The full picture and applications

  • Circles ∣z∣=r|z| = r map to confocal ellipses with foci at ±2\pm 2:

foci at ±A2−B2=±(r+1r)2−(r−1r)2=±4=±2.\text{foci at } \pm\sqrt{A^2 - B^2} = \pm\sqrt{\left(r+\frac{1}{r}\right)^2 - \left(r - \frac{1}{r}\right)^2} = \pm\sqrt{4} = \pm 2.

All these ellipses share the same foci ±2\pm 2, regardless of rr!

  • Rays arg⁡(z)=θ=const\arg(z) = \theta = \text{const}: here rr varies and θ\theta is fixed. Then u=(r+1/r)cos⁡θu = (r+1/r)\cos\theta, v=(r−1/r)sin⁡θv = (r-1/r)\sin\theta. Eliminating rr gives

u2cos⁡2θ−v2sin⁡2θ=[(r+1r)2−(r−1r)2]=4,\frac{u^2}{\cos^2\theta} - \frac{v^2}{\sin^2\theta} = \left[\left(r+\frac{1}{r}\right)^2 - \left(r - \frac{1}{r}\right)^2\right] = 4,

i.e., confocal hyperbolas with the same foci ±2\pm 2.

So the Joukowski map sends the orthogonal coordinate grid of circles and rays to the orthogonal grid of confocal ellipses and hyperbolas — this is the elliptic coordinate system.

In the wild: The Joukowski map (and its cousins z+c/zz + c/z) are the foundation of Joukowski airfoil theory in aerodynamics — a circle in the zz-plane maps to a wing-shaped profile in the ww-plane, and potential flow (which is governed by harmonic functions / holomorphic maps) around a circle can be pulled back to give lift calculations around an airfoil. This is a triumph of conformal mapping.

Source: Classical complex analysis folklore; see Stein–Shakarchi Complex Analysis Ch. 8, or Basic Complex Analysis

Type: Complex AnalysisSource: Classical complex analysis folklore; see Stein–Shakarchi Complex Analysis Ch. 8, or Basic Complex AnalysisEdit on GitHub ↗