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- W2912105334 abstract "Dynamic stall constitutes a major limiting factor for helico-pter's forward speed. Calculations of rotor airloads and helicopter limiting speeds introducing the blade pitching oscillations effects, translate the real case into a reasonable analytical model. The present technique offers a reliable mean for calculating the rotor airloads with the unsteady effects. The method is extended to determine the limiting forward speed of helicopter." @default.
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- W2912105334 date "1985-05-01" @default.
- W2912105334 modified "2023-09-26" @default.
- W2912105334 title "DYNAMIC STALL EFFECTS ON HELICOPTER PERFORMANCE" @default.
- W2912105334 doi "https://doi.org/10.21608/asat.1985.26480" @default.
- W2912105334 hasPublicationYear "1985" @default.
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