@techreport{oai:jaxa.repo.nii.ac.jp:00041134,
 author = {奥山, 政広 and 岩崎, 昭人 and 藤田, 敏美 and 藤枝, 郭俊 and 高橋, ひとし and 玉置, 元昭 and 宮下, 純一 and Okuyama, Masahiro and Iwasaki, Akihito and Fujita, Toshimi and Fujieda, Hirotoshi and Takahashi, Hitoshi and Tamaki, Motoaki and Miyashita, Junichi},
 month = {Nov},
 note = {成層圏プラットホームを想定したパラグライダーが考案され、そのパラグライダーの基本空力特性を把握するために、縮尺が8%程度になる実長翼幅1.2mの模型が製作された。この模型は、傘前縁部の空気取り入れ口がなく、閉じた前縁になっていて、翼型を維持するために、傘内部に圧縮空気を封入している。風洞試験は、2m×2mの固定壁測定部を持つ風洞において、風速を10m/sにして実施された。傘を拘束した状態および非拘束にした状態で模型の空力特性を取得し、また傘の変位を測量した。その結果、模型の基本的な6分力特性が得られ、この特性から本パラグライダー模型の挙動を理解することができた。, A paraglider has been designed for a platform in the stratosphere. To obtain the basic aerodynamic characteristics of the designed paraglider, paraglider models with a real span of 1.2 m were manufactured on a scale of about 8 percent. The leading edge of the canopy of this model is closed and the closed canopy is filled with compressed air to maintain the shape of the aerofoil section. The tests were conducted in the NAL (National Aerospace Laboratory) 2 m x 2 m Gust Wind Tunnel with closed test section at a wind speed of 10 m/s. On the tests, the canopies were conditioned for a bound and unbound strut. Both the forms of the bound and unbound canopies were used to obtain the aerodynamic characteristics and the form of the unbound canopy was used to observe shift of the canopy. As a result, the basic aerodynamic characteristics of the models were obtained, and behavior of the model could be interpreted by the characteristics., 資料番号: AA0004155000, レポート番号: NAL TM-671},
 title = {空気封入式パラグライダー模型の風試結果について},
 year = {1994}
}