Computational aeroelasticity


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.