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Optimal Design of Rotor Blade for a Winged Compound Helicopter at High Advance Ratio

Masahiko Sugiura, Hideaki Sugawara, Yasutada Tanabe, Japan Aerospace Exploration Agency
Kuniyuki Takekawa, Ryoyu Systems

October 10, 2020

https://doi.org/10.4050/F-0076-2020-16454



Optimal Design of Rotor Blade for a Winged Compound Helicopter at High Advance Ratio

  • Presented at Forum 76
  • 8 pages
  • SKU # : F-0076-2020-16454
    • Aircraft Design

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Optimal Design of Rotor Blade for a Winged Compound Helicopter at High Advance Ratio

Authors / Details:
Masahiko Sugiura, Hideaki Sugawara, Yasutada Tanabe, Japan Aerospace Exploration Agency
Kuniyuki Takekawa, Ryoyu Systems