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-771
一般注記This report describes numerical schemes used in the computer program for nozzle performance predications of liquid rocket engines. The program is a set consisting of the following four programs: a program of one-dimensional equilibrium flow(ODE), a one-dimensional kinetic flow(ODK), a two-dimensional kinetic flow(TDK), and a turbulent boundary layer(TBL). Published programs were utilized for ODE and TBL, but the programs for ODK and TDK were newly developed. In the TDK program, an efficient numerical scheme for a two-dimensional nonequilibrium flow was devised for rocket nozzle flowfields, and is described in detail in this report. Computational results are presented for hydrogen/oxygen and NTO/A-50 propellant engines, showing the utility of the present computer program by comparing it with available experimental data.
資料番号: NALTR0771000
レポート番号: NAL TR-771
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45029&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