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ロケットノズルの性能予測計算法
https://jaxa.repo.nii.ac.jp/records/45029
https://jaxa.repo.nii.ac.jp/records/45029e3f39d92-5f64-4e37-9f6a-481605285424
名前 / ファイル | ライセンス | アクション |
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naltr00771.pdf (1.5 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ロケットノズルの性能予測計算法 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
著者 |
中橋, 和博
× 中橋, 和博× 宮島, 博× 木皿, 且人× 毛呂, 明夫× NAKAHASHI, Kazuhiro× MIYAJIMA, Hiroshi× KISARA, Katsuto× MORO, Akio |
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著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所角田支所 | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
著者所属(英) | ||||||
en | ||||||
Kakuda Branch Office, National Aerospace Laboratory(NAL) | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所報告 en : Technical Report of National Aerospace Laboratory TR-771 巻 771, p. 22, 発行日 1983-07 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 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. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0771000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL TR-771 |