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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

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

  • Presented at Forum 76
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  • SKU # : 76-2020-0223-Sugiura
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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

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