Distance fields finds a lot of applications recently in computational geometry. We propose an algorithm to extract the mean camber line of an airfoil using distance fields. This method does not require computing any geometric approximations in- side the airfoil geometry. It also does not need the airfoil coordinates to be evenly distributed on the top and bottom. All the computations are done on a simple Cartesian mesh and can be easily coupled with any existing computational fluid dynamics codes. We show the efficiency of the algorithm on a variety of airfoil geometries. We demonstrate the robustness and exibility of the algorithm for a wide range of airfoil geometries.
|Place of Publication||Delft|
|Publisher||Delft University of Technology|
|Number of pages||15|
|Publication status||Published - 2020|
|Name||Reports of the Delft Institute of Applied Mathematics|