Parallel adaptive finite element Euler flow solver for rotary wing aerodynamics

We discuss the development of a code for the automated reliable numerical simulation of rotor aerodynamics. The code performs all the stages of the analysis--finite element solution, error indication, mesh adaptation--in a parallel multiple-instruction/multiple-data environment making use of efficient scalable parallel algorithms. The main features of all the building blocks of the implemented approach are detailed and discussed. The capabilities and performance characteristics of the parallel automated adaptive procedure are demonstrated with regard to subsonic and transonic compressible how problems. In particular, different hovering rotor problems are analyzed, and the results are compared with experimental data showing good agreement.