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- W23555013 abstract "In the framework of the AIM project the near field of the blade tip vortex of a full-scale helicopter in simulated hover flight was investigated by combining three-component Particle Image Velocimetry and Background Oriented Schlieren measurements. The velocity field measurements in the range of wake ages of ({uppsi _{mathrm{{v}}}={1}^circ }) to ({30}^circ ) in azimuth provided a reference for a quantitative analysis of the Schlieren results yielding vortex core density estimates. Ongoing vortex roll-up was observed at ({uppsi _{mathrm{{v}}}={1}^circ }) while considerable aperiodicity was persistent thereafter. The vortex parameters for ({uppsi _{mathrm{{v}}}>{1}^circ }) were consistent with the Scully vortex model. The particular challenges of full-scale, outdoor testing, especially the limited spatial resolution and aperiodicity effects, resulted in elevated measurement uncertainty as compared to sub-scale experiments." @default.
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- W23555013 date "2013-01-01" @default.
- W23555013 modified "2023-09-24" @default.
- W23555013 title "Towards In-Flight Measurements of Helicopter Blade Tip Vortices" @default.
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- W23555013 doi "https://doi.org/10.1007/978-3-642-34738-2_11" @default.
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