DocumentCode
2655236
Title
Trailing vortex detection and quantitative evaluation of vortex characteristics by PIV technique
Author
Albano, Floriana ; De Gregorio, Fabrizio ; Ragni, Antonio
Author_Institution
Itlian Aerosp. Res. Center, CIRA, Capua, Italy
fYear
2003
fDate
25-29 Aug. 2003
Firstpage
31
Lastpage
43
Abstract
This paper summarises the activities performed in order to investigate the formation, motion and persistence of trailing vortices released by large commercial aircraft. Two different experimental test campaigns were carried out in two different large towing tank facilities performing PIV measurements. The lesson learned by the first investigation and by the experience of the scientific community, the solution adopted in order to characterise the wake vortex by the initial formation phase down to wake collapsing in the far-wake region are illustrated. Together with the adopted technical solution, with the selected experimental facility and with the improved measurement system, a particular care is taken: on the data analysis description, on the importance of advanced PIV algorithms and on the selected postprocessing methods for evaluating the main magnitudes characterising the vortex structures.
Keywords
aircraft; data acquisition; data analysis; velocity measurement; vortices; wakes; PIV algorithms; PIV measurements; aircraft; data analysis; particle image velocimetry; quantitative evaluation; trailing vortex detection; wake vortex; Aerospace testing; Aircraft; Coordinate measuring machines; Frequency measurement; Length measurement; Motion measurement; Particle measurements; Performance evaluation; Streaming media; Velocity measurement;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on
Print_ISBN
0-7803-8149-1
Type
conf
DOI
10.1109/ICIASF.2003.1274850
Filename
1274850
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