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In this paper,the effects of turbulence on sound generation and velocity fluctuations due to pressure waves in a large subsonic wind tunnel are studied.A trip strip located at different positions in the contraction part or at one position in the diffuser of a large wind tunnel is used to investigate the aforementioned phenomenon,and the results indicate that the trip strip has significant effects on sound reduction.The lowest turbulence intensity and sound are obtained from a trip strip with a diameter of 0.91mm located either at X/L = 0.79 or at X/L = 0.115 in the wide portion of the contraction.Furthermore,the effect of monopole,dipole and quadrupole sources of aerodynamic noise at different velocities is investigated,and it is demonstrated that the contribution of the monopole is dominant,while the shares due to the dipole and quadrupole remain less important.In addition,it is found that the sound waves have a modest impact on the measured longitudinal turbulence and are generated essentially by eddies.
In this paper, the effects of turbulence on sound generation and velocity fluctuations due to pressure waves in a large subsonic wind tunnel are studied. A trip strip located in different positions in the contraction part or at one position in the diffuser of a large wind tunnel is used to investigate the current phenomenon, that the the trip strip has significant effects on sound reduction. The lowest turbulence intensity and sound are obtained from a trip strip with a diameter of 0.91mm located either at X / L = 0.79 or at X / L = 0.115 in the wide portion of the contraction. Focus further, the effect of monopole, dipole and quadrupole sources of aerodynamic noise at different velocities is investigated, and it is demonstrated that the contribution of the monopole is dominant, while the shares due to the dipole and quadrupole remain less important.In addition, it is found that the sound waves have a modest impact on the measured longitudinal turbulence and are generated e ssentially by eddies.