Click here
to see a short animation of the evolution of the pressure field on a
twisting NACA airfoil.
The following seven slides, taken from a CSAR poster presented in
October 2005, summarize some recent results of the comparative
assessment of load transfer schemes along curved fluid/structure
interfaces with non-matching discretizations. The key emphasis of this
analysis is to determine the effect of the curvature in the error
associated with the load transfer.