Research Article
Computational Study of a Transverse Rotor Aircraft in Hover Using the Unsteady Vortex Lattice Method
Figure 5
Evolution of the wake structure with (a, b, and c) and without (d, e, and f) root vorticity (RV) for the case .
| (a) 3 revs. RV |
| (b) 6 revs. RV |
| (c) 9 revs. RV |
| (d) 3 revs. |
| (e) 6 revs. |
| (f) 9 revs. |