Abstract
One of the most important noise sources in low Mach number flows is the result of a blade moving through a region of unsteady flow or turbulence. The mechanism that causes the sound that radiates to the acoustic far field is referred to as leading edge noise. There are many examples where this sound source occurs including fans of all types, helicopter rotors and propellers. This chapter discusses the mechanisms of leading edge noise and shows how it can be calculated for a stationary blade in a uniform flow.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
