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.
논문 기본 정보
- 자료유형
- 학술대회자료
- 저자정보
- 발행연도
- 2023.11
- 수록면
- 2,482 - 2,487 (6page)
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초록· 키워드
오류제보하기
Traditional aircraft face limitations in dynamically adjusting wing lengths in constrained settings to reap aerodynamic benefits and spatial efficiencies. Moreover, in-flight self-repairs for wing damages induced by external circumstances are unfeasible. Addressing these issues, this paper introduces two distinct mechanisms: a balloon-assisted inflatable wing at the end of the wings and another based on the "multistable inflatable origami structures." The former offers dynamic wing length adjustments in space-restricted urban environments, while the latter, with its multistable inflatable origami design, allows the detachment of a damaged wing and its replacement with an inflated origami-style wing. To realize these two mechanisms, directing fluid through the main wing is imperative. The paper proposes the use of an S duct as a solution and presents the design of both the S duct and a UAV platform. The feasibility of these mechanisms has been substantiated through mathematical equations for aircraft design and Computational Fluid Dynamics (CFD) analysis using Ansys.
목차
Abstract
1. 서론
2. 이론 및 실험
3. 성능 검증
4. 결론
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