Publikationsdatum:
2011-08-16
Beschreibung:
Some results are described for a lifting rectangular wing centrally located on a circular-cylindrical body. This simple configuration has been utilized in order to assess the merits of a mapping technique for wing-body configurations. The procedure employed makes use of a coordinate transformation to simplify specification of the surface boundary condition in the computation of the flow about the wing. The method can be extended to incorporate wing sweep, finite length body of noncircular cross section, and arbitrary wing placement; however, these extensions involve a considerable increase in complexity of the problem.
Schlagwort(e):
AERODYNAMICS
Materialart:
Journal of Aircraft; 11; Apr. 197
Format:
text
