Skip to main content

Section 19.3 Contour integrals

Introduction goes here.
  • A contour integral is just a line integral over a curve \(C\) in the complex plane:
    \begin{equation*} \int_{C} f(z)\dd{z} \end{equation*}
    We evaluate it by parametrizing \(C\text{:}\)
    \begin{equation*} \int_{a}^{b} f(z(t))z'(t)\dd{t} \end{equation*}
  • Great example to go through: if \(C\) is the unit circle parametrized counterclockwise, and \(n\neq-1\) is an integer, then
    \begin{equation*} \int_{C} z^{n}\dd{z}=0\text{.} \end{equation*}
    However, as an exception,
    \begin{equation*} \int_{C} \frac{1}{z}\dd{z}=2\pii\ii\text{.} \end{equation*}
  • Suppose that \(\bv F(x,y)=(P(x,y),Q(x,y))\) is the Pólya vector field of the function \(f(z)=P(x,y)-\ii Q(x,y)\text{.}\) Then:
    \begin{align*} \oint_C f(z)\dd{z} \amp = \oint_C (P-\ii Q)(\dd{x}+\ii\dd{y})\\ \amp = \qty(\oint_C P\dd{x}+Q\dd{y})+\ii\qty(\oint_C P\dd{y}-Q\dd{x})\\ \amp = \qty(\oint_C\bv F\cdot\uv{t}\dd{s})+\ii\qty(\oint_C\bv F\cdot\uv{n}\dd{s}) \end{align*}
    Thus the contour integral computes BOTH the circulation AND the flux at the same time!
  • Winding number?
  • Blasius’s theorem: The force experienced by a two-dimensional fixed body in a steady irrotational flow is given by
    \begin{equation*} L-\ii D=\frac{\ii\rho}{2}\oint_C \qty(\dv{w}{z})^2\dd{z}\text{,} \end{equation*}
    where \(w(z)=\phi(x,y)+\ii\,\psi(x,y)\) is the complex potential of the flow, \(C\) is a contour enclosing the body, and \(\rho\) is the fluid density. Here, \(L\) is the lift and \(D\) is the drag. (Note the conjugate.)
    Furthermore, the moment about the origin is given by
    \begin{equation*} M=\RE\qty{-\frac{\rho}{2}\oint_C z\qty(\dv{w}{z})^2\dd{z}}\text{.} \end{equation*}