Mechanics of flow-induced sound and vibration
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...In the limit for low-frequency dipole noise, where the acoustic wavelength is much larger than the airfoil chord, the sin(2)(θ/2) term changes into sin(2)(θ) [5,33]....
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...For trailing edge noise, L is usually taken to be the boundary layer thickness at the trailing edge [5,6], although a recent study suggests that a constant reference length should be used [12]....
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...wind turbines, airplanes, helicopters, fans), the characteristics of airfoil noise have been investigated extensively in both experimental and theoretical studies [3-13]....
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...For inflow-turbulence noise radiated from the leading edge the θ-dependence is inverted [5,11] and θ should be replaced by (π-θ)....
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...2 Trailing edge bluntness noise When the trailing edge thickness of an airfoil is larger than about 20% of the boundary layer displacement thickness, trailing edge bluntness noise can occur [5,6,12]....
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