Ramer–Douglas–Peucker algorithm

Generally speaking, for low-speed flow around an aerofoil, the largest gradients in the flow-properties coincide with the greatest curvature of the aerofoil, and thus are the region that requires the greatest concentration of cells (or nodes) in the computational domain. Many of the simplified treatments for spacing points along an aerofoil use a logarithmic spacing… Continue reading Ramer–Douglas–Peucker algorithm

Categorised as Blog Tagged