並列タイトル等Numerical Simulations of Flow Around ATP Engine
タイトル(掲載誌)航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory SP-9
一般注記Flow fields around the ATP engine with counter-rotating propeller are simulated numerically by solving three-dimensional unsteady Euler equations. The numerical method is implicit approximate factorization developed by Beam and Warming. The calculation model is UDF style engine with 8 by 8 SR-3 propellers. The distribution of pressure on the blade surfaces, the propeller efficiencies, and the velocity vectors downstream of propellers are obtained. The relation of propeller efficiencies and velocity vectors downstream of rear propellers shows the features of counter-rotating propellers.
資料番号: NALSP0009036
レポート番号: NAL SP-9
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43327&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