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Rotor Aerofoil Design for Lynx Helicopter by durak89 is a document available to read on EtoBox.

What is Rotor Aerofoil Design for Lynx Helicopter about?

The document discusses rotor aerofoil design requirements for helicopters operating at high speeds. It focuses on the Lynx helicopter as a case study. Key points: 1) Rotor blades experience high incidences on the retreating side and high Mach numbers on the advancing side at high speeds, limiting forward flight. 2) The Lynx rotor uses three customized aerofoils - the RAE 9645, a cambered, high-lift section between 65-85% span; the RAE 9648, a reflexed section inboard to balance moments; and the RAE 9634

Author

durak89

Language

EN