並列タイトル等A Hypersonic Thermally-Nonequilibrium Reacting Flow around a 3-Dimensional Blunt Body
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-10
一般注記This work deals with a flow around a re-entry hypersonic vehicle or AFE vehicle at flight speed Mach=31.6 under a thermally and chemically non-equilibirium concept. As a thermally non-equilibrium model, we adopt Park's two-temperature model; translational and vibrational temperatures or molecules. And as a chemically reacting model, the modified Arrhenius form is used, where all the reaction rates depend on both temperatures. Because of the reaction delay, the distance between peripheral shock wave and the body increases from one-temperature model. Under this concept, the reaction front is significantly separated from the shock front; the reaction delay time is accurately given by the present shock fitting method.
資料番号: NALSP0010011
レポート番号: NAL SP-10
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=43340&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