Research Article
Helicopter Rotor Flow Analysis Using Mapped Chebyshev Pseudospectral Method and Overset Mesh Topology
Figure 14
Surface pressure coefficients at the radial locations of 0.5, 0.68, 0.8, 0.89, and 0.96 at Mach number of 0.439.
(a) |
(b) |
(c) |
(d) |
(e) |