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- W187819878 abstract "In the past, significant effort was placed in flow field measurementsof rotor wake vortices. This was driven by the importance of the rotorblade tip vortices for the blade-vortex interaction noise radiation ofhelicopters. The goal is to obtain reliable data for the generation ofa generalized model of tip vortices, including their generation androll-up, and their aging while passing through the rotor disk andinteracting with some of the revolving blades. In 2001 DLR, ONERA,NASA Langley, US Army AFDD and DNW performed the HART II test in thelarge low-speed facility of the DNW with a 40% Mach scaled model rotorof the Bo105. Major emphasis was placed on three component particleimage velocimetry (3C-PIV) measurements of the blade tip vortices. Theywere traced from their creation in the second and third quadrant of therotor disk to the rear of the rotor, including blade-vortex interaction(BVI). This paper deals with difficulties associated with the analysisof such 3C-PIV measurements and with the methodologies that need to beapplied to overcome these difficulties." @default.
- W187819878 created "2016-06-24" @default.
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- W187819878 date "2005-01-01" @default.
- W187819878 modified "2023-09-27" @default.
- W187819878 title "Analysis methodology for 3C PIV data" @default.
- W187819878 hasPublicationYear "2005" @default.
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