Flying wing concept for regional transport

Autor:	Pambagjo, Tjoetjoek Eko, Nakahashi, Kazuhiro
Jazyk:	angličtina
Rok vydání:	2002
Předmět:	flying wing 空力係数 全翼機 payload regional transport aircraft configuration GeneralLiterature_MISCELLANEOUS 地域輸送 アスペクト比 ペイロード aerodynamic coefficient aspect ratio 航空機設計 航空機配置 ComputingMethodologies_COMPUTERGRAPHICS aircraft design
Zdroj:	航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集 = Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001. 53:233-238
ISSN:	0289-260X
Popis:	The flying wing is regarded as an alternate configuration to reduce drag and structural weight. This paper presents the design process of a medium size Blended-Wing-Body airplane, which in essence is a flying wing configuration. Because of the rapid changing of thickness and chord distribution, it requires special design tools. In the present study the wing surface is generated using RAPID method. Takanashi's inverse design method is utilized to obtain the airfoil shape. The required target pressure distribution is specified using constrained target pressure specification techniques. The present study shows that the design difficulties can be overcome by using the proposed design tools. 資料番号: AA0032819040 レポート番号: NAL SP-53
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=jairo_______::be97cef0bade8b5bad7c560f0725dd16 http://id.nii.ac.jp/1696/00038070/ Zobrazit plný text záznamu