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
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-677
一般注記In order to improve the weather cock stability derivative Cnβ of the NAL STOL research aircraft model, some surveys of the flow field around the empennage for the STOL landing configuration were carried out. The down wash angle, the side wash angle, and the dynamic pressure at the aerodynamic center of the empennage (25% mean aerodynamic chord) were obtained by means of linear interpolation of the values measured at the two sections perpendicular to the free stream. Effects of the engine thrust coefficient and the two types of vortex generator on the flow field, and the directional stability in the case of an inner engine becoming inoperative, were studied with reference to the results of the force tests.
資料番号: NALTR0677000
レポート番号: NAL TR-677
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=44934&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