著者・編者STOLプロジェクト推進本部実験機開発室空力技術開発チーム
Aerodynamics Team Research Aircraft Development Section STOL Aircraft Project Group
並列タイトル等Low-Speed Wind Tunnel Tests of the NAL Fan-Jet STOL-Research-Aircraft Model with Ground Simulation by Tangential Blowing
タイトル(掲載誌)航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-828
一般注記To investigate the basic aerodynamic characteristics of the turbofan powered-lift STOL aircraft near the ground, wind tunnel tests were made on the 8% NAL Quiet STOL Research Aircraft complete model with an upper surface blowing flap system in the NAL 6.5m×5.5m low speed wind tunnel. The wind tunnel tests were conducted using a fixed ground plane with tangential blowing boundary-layer control instead of a moving belt ground plane. The tests covered the effects on longitudinal and lateral static stability produced by variations of flap angle and engine thrust, and by ground proximity. Some of the more significant effects of ground proximity include appreciable changes in six-component force and moment once jet impingment occured. These data obtained in the wind tunnel tests were offered for analysis of flying qualities of the NAL Quiet STOL Research Aircraft.
資料番号: NALTR0828000
レポート番号: NAL TR-828
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45086&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