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- W40549721 abstract "ABSTRACT This paper surveys the historical perspective and design considerations for developing the human powered aircraft(HPA). Especially the weight and material s, aerodynamics, flight controls, and power trains are focused. The average power a hum an can produce and sustain is approximately 200∼250 W which is a critical design constraint of HPA. The survey shows that the empty weight of HPA was in the 30 ∼40 kg range(90∼110 kg include pilot). Thus, in order to design a successful HPA, the value of power to weight ratio should be 2.0 W/kg or above. The HPA design technique could be applied directly to the development of an unmanned high altitude airplanes used for atmospheric research, where light structures, low Reynolds number aerodynamics and high efficiency propeller design are required as well. Key Words : Human Powered Aircraft(인력비행기), Muscular Engine(근육엔진), Low Reynolds Number Aerodynamics(저레이놀즈수 공기역학), Minimum Induced Loss Propellers(최소유도손실 프로펠러) 2009년 3월 11일 접수 ~ 2009년 3월 26일 심사완료* 해군사관학교 기계조선공학과** 공군사관학교 항공우주공학과 연락저자, E-mail : kylee04@hanmail.net 경상남도 진해시 앵곡동 사서함 88" @default.
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- W40549721 date "2009-01-01" @default.
- W40549721 modified "2023-09-24" @default.
- W40549721 title "The Design and Construction Consideration for Developing the Human Powered Aircraft" @default.
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