Development of an indicial function approach for the two-dimensional incompressible/compressible aerodynamic loadmodelling

By using a combined analytical–computational methodology, a unified modelling of aerodynamic indicial functions covering the incompressible, subsonic compressible, transonic, and supersonic flight speed regimes is presented. The procedure is carried out in conjunction with a computational fluid dynamic analysis. For a plunging–pitching airfoil, selected unsteady aerodynamic load expressions have been supplied, and appropriate procedures enabling one to obtain these loads via the indicial function approach have been presented. While a single indicial function is needed to describe the aerodynamic loads in the incompressible flight speed regime, for cases where the compressibility effects play a dominant role, four indicial functions areneeded.Having inview theusefulnessof indicial functions towardsdeterminationofunsteady aerodynamics loads in both time and frequency domains, and implicitly for aeroelastic response andflutter predictions, the advantages of their implementation anduse appear evident. Comparisons and validations of the aerodynamicmodel against numerical, analytical, and experimental results are presented, and pertinent conclusions are drawn.