A Simple Analytical Model for Investigation of Fuselage-Rotor Interference

[PDF] aiaa.org

Slowed hingeless rotor wind tunnel tests and validation at high advance ratios

X Wang, A Bauknecht, S Maurya, I Chopra - Journal of Aircraft, 2021 - arc.aiaa.org
In forward flight, slowing down a rotor alleviates compressibility effects on the advancing
side blade tip, extending the cruise speed limit, and inducing high-advance-ratio flight …
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[引用][C] Development of a blade element method for CFD simulations of helicopter rotors using the actuator disk approach

DV Leza - 2018 - Master's thesis, Delft University of …
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