並列タイトル等Flight Investigation on Stall Characteristics of a Light Airplane Equipped with a BLC System
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Flight tests were conducted using a light airplane to investigate the effect of high lift devices upon stall speed.The “1-g-break Technique” was used for determining the stall speed.Test configurations were(1)modified configuration by incorporating slats as well as the boundary layer control on flaps and flaperons and(2)the same configuration less slats installation.The results were compared with the original configuration.For each test configuration,lift coefficients corresponding to the stall speeds obtained were plotted against flap setting angle with various test parameters such as power setting,suction capacity and flaperon droop angle.The flight test results were compared with wind turnel test data.
資料番号: NALTM0278000
レポート番号: NAL TM-278
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