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A PROCEDURE FOR THE EVALUATION OF INSTALLED PROPELLER NOISE

2001

Abstract A method for the prediction of the acoustics of a propeller in the flow-field of a wing is presented. The method is used to study the noise generated by the unsteady loading induced on the propeller as it passes through the wing flow-field. Both the aerodynamic and acoustic methods are previously proven techniques, the aerodynamic method being based on a combination of free wake analysis and a three-dimensional boundary element method, while the acoustic calculation is a full-surface, moving medium form of the Ffowcs Williams–Hawkings equation. Calculations are presented for a reference case of a four-bladed low-speed propeller in forward flight. The acoustic predictions are supple…

EngineeringAcoustics and Ultrasonicsbusiness.industryMechanical EngineeringAcousticsPropellerAerodynamicsCondensed Matter PhysicsNoiseMechanics of MaterialsPropulsorRetarded timeAeroacousticsAcoustic radiationbusinessStructural acousticsJournal of Sound and Vibration
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