where is a complex variable in the new space and is a complex variable in the original space.
This transform is also called the Joukowsky transformation, the Joukowski transform, the Zhukovsky transform and other variations.
In aerodynamics, the transform is used to solve for the two-dimensional potential flow around a class of airfoils known as Joukowsky airfoils. A Joukowsky airfoil is generated in the complex plane (-plane) by applying the Joukowsky transform to a circle in the -plane. The coordinates of the centre of the circle are variables, and varying them modifies the shape of the resulting airfoil. The circle encloses the point (where the derivative is zero) and intersects the point This can be achieved for any allowable centre position by varying the radius of the circle.
Joukowsky airfoils have a cusp at their trailing edge. A closely related conformal mapping, the Kármán–Trefftz transform, generates the much broader class of Kármán–Trefftz airfoils by controlling the trailing edge angle. When a trailing edge angle of zero is specified, the Kármán–Trefftz transform reduces to the Joukowsky transform.
The complex velocity around the airfoil in the -plane is, according to the rules of conformal mapping and using the Joukowsky transformation,
Here with and the velocity components in the and directions respectively ( with and real-valued). From this velocity, other properties of interest of the flow, such as the coefficient of pressure and lift per unit of span can be calculated.
A Joukowsky airfoil has a cusp at the trailing edge.
The transformation is named after Russian scientist Nikolai Zhukovsky. His name has historically been romanized in a number of ways, thus the variation in spelling of the transform.
Example of a Kármán–Trefftz transform. The circle above in the -plane is transformed into the Kármán–Trefftz airfoil below, in the -plane. The parameters used are: and Note that the airfoil in the -plane has been normalised using the chord length.
The Kármán–Trefftz transform is a conformal map closely related to the Joukowsky transform. While a Joukowsky airfoil has a cusped trailing edge, a Kármán–Trefftz airfoil—which is the result of the transform of a circle in the -plane to the physical -plane, analogue to the definition of the Joukowsky airfoil—has a non-zero angle at the trailing edge, between the upper and lower airfoil surface. The Kármán–Trefftz transform therefore requires an additional parameter: the trailing-edge angle This transform is
where is a real constant that determines the positions where , and is slightly smaller than 2. The angle between the tangents of the upper and lower airfoil surfaces at the trailing edge is related to as
The derivative , required to compute the velocity field, is
First, add and subtract 2 from the Joukowsky transform, as given above:
Dividing the left and right hand sides gives
The right hand side contains (as a factor) the simple second-power law from potential flow theory, applied at the trailing edge near From conformal mapping theory, this quadratic map is known to change a half plane in the -space into potential flow around a semi-infinite straight line. Further, values of the power less than 2 will result in flow around a finite angle. So, by changing the power in the Joukowsky transform to a value slightly less than 2, the result is a finite angle instead of a cusp. Replacing 2 by in the previous equation gives
which is the Kármán–Trefftz transform. Solving for gives it in the form of equation A.
^Joukowsky, N. E. (1910). "Über die Konturen der Tragflächen der Drachenflieger". Zeitschrift für Flugtechnik und Motorluftschiffahrt (in German). 1: 281–284 and (1912) 3: 81–86. CS1 maint: discouraged parameter (link)