An interpolation method, namely using splines, for two dimensional flows is presented. The potential flow was obtained as the superposition of an undisturbed flow and a flow generated by a doublet distribution at the wing surface and in the wake.
In Von Karman Inst. for Fluid Dyn. Numerical Methods in Fluid Dyn. 23 p (SEE N79-27448 18-34
- Pub Date:
- Computational Fluid Dynamics;
- Two Dimensional Flow;
- Wing Flow Method Tests;
- Three Dimensional Flow;
- Fluid Mechanics and Heat Transfer