Computation of potential flows with embedded vortex rings and applications to helicopter rotor wakes
Abstract
A finite difference scheme for solving the motion of a number of vortex rings is developed. The method is an adaptation of the 'cloud-in-cell' technique to axisymmetric flows, and is thus a combined Eulerian-Lagrangian technique. A straightforward adaptation of the cloud-in-cell scheme to an axisymmetric flow field is shown to introduce a grid dependent self-induced velocity to each vortex ring. To correct this behavior the potential is considered to consist of two parts, a local and a global field. An improved difference formula is derived, allowing the accurate calculation of the potential at points near vortex locations. The local potential is then subtracted before calculating the velocity, leaving only the influences of the remaining vortices. The correct self-induced velocity is then explicitly added to the vortex velocity. Calculations of the motion of one and two vortex rings are performed, demonstrating the ability of the new method to eliminate the grid dependence of the self-induced velocity. The application of the method to the calculation of helicopter rotor flows in hover is attempted.
- Publication:
-
NASA STI/Recon Technical Report N
- Pub Date:
- September 1983
- Bibcode:
- 1983STIN...8417526R
- Keywords:
-
- Computational Fluid Dynamics;
- Helicopter Wakes;
- Potential Flow;
- Rotary Wings;
- Vortex Rings;
- Computational Grids;
- Finite Difference Theory;
- Flow Equations;
- Flow Velocity;
- Hovering;
- Problem Solving;
- Fluid Mechanics and Heat Transfer