Unsteady transport mechanisms in an axial turbine

A numerical analysis using a commercial unsteady Navier-Stokes solver has b een performed on a pin/blade configuration, in order to assess the efficacy of a commercial code in calculating time-periodic interactions and to gain a better understanding of the unsteady flow physics in axial turbines. Two cases have been investigated, with the pin positioned at 25 and 50 percent of true chord ahead of the leading edge. Both configurations have been com puted both two and three dimensionally. The two-dimensional case was used t o examine the influence of numerical parameters, such as mesh, time, and sp ace discretization. The three-dimensional case allowed insight into the com plete flow field including the wake influence on the secondary flow and mix ing process of the blade row. The basic mechanisms of the wake-blade intera ction proved, as expected, to be the same for both pin positions. Yet, as t he closest pin wake interaction with the blade field was much stronger, its features have helped to identify the respective roles of wake fluid transp ort and blade potential field for both cases. The latter effect, noticeably strong with the thick leading edge blade form presented in this study, has often been neglected and this study helps shed new light on this phenomeno n. The code used had been validated in previous work for pin-free steady fl ow within the same blade row and the new time-dependent case has sewed to c onfirm the code range and limitations. [S0889-504X(00)02104-8].