並列タイトル等Moving belt ground effect testing system of NAL 6.5 x 5.5 m low speed wind tunnel
タイトル（掲載誌）航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory
一般注記航空機模型の離着陸時の地面効果を評価するために、ムービングベルト式の地面効果試験装置が1995年3月に大型低速風洞に完成した。ここでは、本装置の構成と特性について述べる。
A moving belt type ground effect measurement system was constructed to evaluate ground effect characteristics of aircraft models at the NAL low speed wind tunnel facility in March 1995. This paper summarizes the hardware and function of this equipment. Some function tests and flow characteristic tests were carried out, with this equipment installed in the test section. Some effects of the following parameters to drive this system on the flow above the belt plane are indicated: (1) belt running speed; (2) boundary layer suction; and (3) rear flap of ground plane. These parameters were adjusted to the optimum values experimentally. Some experimental results on the following items are indicated: (1) static pressure distribution along the wind tunnel axis on the moving plane; (2) turbulent distribution on the moving plane; and (3) boundary layer velocity profile on the moving plane.
資料番号: AA0001439000
レポート番号: NAL TM-724
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=40182&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ