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- W857536135 abstract "Calculated and measured values of helicopter rotor flapping angles in forward flight are compared for a model rotor in a wind tunnel and an autogiro in gliding flight. The lateral flapping angles can be accurately predicted when a calculation of the nonuniform wake-induced velocity is used. At low advance ratios, it is also necessary to use a free wake geometry calculation. For the cases considered, the tip vortices in the rotor wake remain very close to the tip-path plane, so the calculated values of the flapping motion are sensitive to the fine details of the wake structure, specifically the viscous core radius of the tip vortices." @default.
- W857536135 created "2016-06-24" @default.
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- W857536135 date "1981-04-01" @default.
- W857536135 modified "2023-10-14" @default.
- W857536135 title "Comparison of Calculated and Measured Helicopter Rotor Lateral Flapping Angles" @default.
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- W857536135 doi "https://doi.org/10.4050/jahs.26.46" @default.
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