Abstract
In this paper, three components of flow velocity around NACA0012 airfoil in some two dimensional sections are measured by using the stereo P1V method in order to clarify flow structures and unsteady behavior of airfoil tip flows contributed to tip flow noise. The Reynolds number based on the chord length of the airfoil and uniform flow velocity is 1.3×10^5 and 3.3×10^4, and the airfoil is under the high lift condition. Band pass filtered characteristics with velocity distributions are shown.
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 callMore From: The Proceedings of the Fluids engineering conference
Disclaimer: 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.
