A rotor blade for a rotary wing aircraft and a tip for the rotor blade. The rotor blade includes a blade root, a blade tip and a blade body that extends from the blade root to the blade tip. The blade tip includes: a continuously swept leading edge, a compound trailing edge, and a continuous anhedral.
ROTOR BLADE TIP DESIGN FOR IMPROVED HOVER AND CRUISE PERFORMANCE
13.09.2018
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Rotor blade tip design for improved hover and cruise performance
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