Numerical simulations of the sound generation by flow over surface mounted cylindrical cavities including wind tunnel installation effects

摘要

In the context of the AEROCAV French Research Program, Large-Eddy Simulations were conducted to compute the turbulent structures and the noise generated by the flow over realistic cavities, similar to those present on aircraft fuselages and wings. The radiated acoustic field was computed using a Kirchhoff integral method. Two geometrical configurations are considered, both with cylindrical shapes but with different Depth/Diameter aspect ratio (H/D = 1 and H/D = 0.5) embedded in a subsonic flow (Mach = 0.2) and for a Reynolds number based on the length of the cavity equal to 4.6·10~5. Dedicated experimental aerodynamic and aeroacoustic measurements databases are used to validate the numerical computations. Experimental and numerical flows are similar except that the boundary layer upstream the cavity is turbulent in the experiments and laminar for the CFD. The aerodynamic fields in the two sets of results are in good agreement, whereas the acoustic field is largely influenced by the installation effects. These effects are analyzed through computations based on Boundary Element Method and CAA and then corrections factors are provided. The acoustic emission for the H/D = 1 case is characterized by a discrete tonal mode, as a superposition of structural and Rossiter resonance phenomena, while the H/D = 0.5 case presents a directive and highly dissymmetrical broadband noise emission. A numerical process is also proposed to control this dissymmetry.