Two-dimensional interaction of vortices with a blade

David Poling, Demetri P. Telionis

26th Aerospace Sciences Meeting · 1988 · 18 citations · 4 references

Concepts

Abstract

The problem of blade-vortex interaction is studied experimentally and numerically. Vortices are generated in the laboratory by pitching an airfoil upstream of the model. LDV measurements are obtained in the neighborhood of the leading edge of the airfoil. Ensemble-averaged velocity vector fields and vorticity contours are thus constructed. A vortex is modeled numerically by a cloud of discrete ideal point vortices. The problem is solved via a Joukowski transformation. The interaction of distributed vorticity with the leading edge of the airfoil is examined.

References

4