Abstract
Ice formation constitutes one of the major challenges to aviation safety, since several accidents have had their origin in this kind of phenomenon. The comprehension of ice accretion on unprotected airfoils, engine intakes, etc. is fundamental from the point of view of both aircraft design and certification requirements since large changes in aerodynamic behaviour and performance take place. The present paper describes tests conducted in a conventional wind tunnel on NACA 0012 airfoils with simulated rime and glaze ice, using laser Doppler velocimetry to measure the flow around the modified airfoils and also the velocity profiles along the viscous wake in order to obtain the drag coefficient. Distortions of the flow field lead to changes in the airfoil aerodynamic characteristics.
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: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
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.
