Blunt trailing edges in a flow often generate tone noise due to wall-jet shear layer and vortex shedding. In this paper, the space-time conservation element (CE/SE) method is employed to numerically study the near-field noise of blunt trailing edges. Two typical cases, namely, flow past a circular cylinder (aeolian noise problem) and flow past a flat plate of finite thickness are considered. The computed frequencies compare well with experimental data. For the aeolian noise problem, comparisons with the results of other numerical approaches are also presented.
Document ID: 20030005099. NASA/CR-2002-212013. NAS 1.26:212013. AIAA Paper 2003-0365. E-13703. 41st Aerospace Sciences Meeting and Exhibit; 6-9 Jan. 2003; Reno, NV; United States.
