A jet from a nozzle whose exit edge is rounded at the inside radiates by far more sound than from a usual sharp edge nozzle. The cause of such increase in the sound emission has been traced to the unsteadiness of flow separation on the (streamwisely-) convex wall. The unsteady behaviour of separation of the flow on a convex wall is profoundly influenced by disturbances in the flow, especially when the disturbance is slight. For a laminar flow with very little disturbances in the flow, the separation point remains quite fixed, while for a flow with a turbulent boundary layer it exhibits considerable fluctuation.
For a flow condition in which the boundary layer is regarded as laminar (in some aspects) but is affected by fair amount of disturbances, the separation point fluctuates violently, and as a result, very remarkable increase in sound emission takes place. Investigation on the mode of fluctuation of the separation point has also been made, in relation to the disturbance characteristics of the flow.
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