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