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- W4312328560 abstract "The flow-field created by a UAV helicopter rotor in steady hover at low-Reynolds numbers is studied by means of particles image velocimetry (PIV). Results are shown for a three-bladed rotor configuration for different pitch angles and RPM settings. Provided is a short description of the rotor test stand and its PIV setup. Precise measurements are achieved for the velocity field and the individual vortex positioning. All results are shown in a convenient form, which allows easy comparison with similar PIV flow-field measurements. Conclusions are drawn on the influence of the power setting of the model helicopter rotor on the flow-field geometric characteristics of the studied rotor configuration." @default.
- W4312328560 created "2023-01-04" @default.
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- W4312328560 date "2022-01-01" @default.
- W4312328560 modified "2023-10-16" @default.
- W4312328560 title "PIV investigation of the influence of the power setting of a UAV helicopter rotor in hover on the flow-field geometry" @default.
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- W4312328560 doi "https://doi.org/10.1063/5.0105571" @default.
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