1. Panel Model with CAD system
Figure 1: CAD model of full car (Full Image)
The model shown above was used to study the influence of an anhedral angle on the wing loading of the front wing and the consequences on the whole underbody flow and resulting loads.
2. VSAERO solution (with free wakes)
Figure 2: Computed surface pressure distribution (Full Image)
Related Material
(on CD-ROM)- About VSAERO Model
- Wings for Racing Cars
- Panel Methods