並列タイトル等Development of Subsonic Computational Aerodynamic Program Using Panel Method
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-3
一般注記This paper presents the Subsonic Computational Aerodynamic Program (SUSCAP) that we have developed as an effective design tool to reduce the cost and time of wind tunnel tests. This code is based on a potential flow Panel Method coupled with a vortex-sheets renewal technique. The main function of the code is aerodynamic coefficient estimation of a three dimensional flying object. Other functions are also added, that is, velocity estimation at arbitrary points apart from the boundary suface, and high subsonic flow simulation by Prandtl-Glauert transformation. In order to investigate the usefulness of the code in designing aerodynamic shapes, this code is applied to a Wing-Boby-Tail configuration and a cruciform missile configuration. Their pressure distributions and roll moments are calculated. Calculated results are compared with the measured data, and the agreement is found satisfactory.
資料番号: NALSP0003020
レポート番号: NAL SP-3
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43162&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