지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
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초록· 키워드
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Human Powered Aircraft (HPA) should be light in weight and have high efficiency because power source of propulsion is human muscles. Airframe structure takes up most of empty weight of aircraft, so weight reduction of structure is very important issue for HPA. In this paper, design/analysis/test procedures for ultra light weight structure of the HPA developed by Korea Aerospace Research Institute (KARI) are explained briefly. Structural design is conducted through case studies on HPA in the USA and Japan. Loads analysis is performed to calculate design loads which is needed for structural design and analysis. Structural analysis is conducted for structure sizing. Static strength test of main wing spar which is primary structure of wing is performed to verify structural integrity.
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등록된 정보가 없습니다.
참고문헌 (6)
참고문헌 신청
Byrne, M / 2010 / Human Powered Aircraft / Aircraft Design Project :1~20
Nakamura, K / 1992 / Human Powered Aircraft of Japan / The Human Powered Aircraft Group Symposium
Oh, S. J / 1999 / The Study of the Main Wing Design and Production for the Man Powered Aircraft / Journal of the Korean Society for Aeronautical and Space Science 27(6):15~16
Cruz, J. / 1989 / Structural Design Conditions for Human Powered Aircraft / OSTIV Conference
Evseev, D. D / ARGON, Multidisciplinary Analytical Support of Aircraft Design
Nakamura, K / 1992 / Human Powered Aircraft of Japan / The Human Powered Aircraft Group Symposium
Oh, S. J / 1999 / The Study of the Main Wing Design and Production for the Man Powered Aircraft / Journal of the Korean Society for Aeronautical and Space Science 27(6):15~16
Cruz, J. / 1989 / Structural Design Conditions for Human Powered Aircraft / OSTIV Conference
Evseev, D. D / ARGON, Multidisciplinary Analytical Support of Aircraft Design
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