複合エンジン燃焼器におけるスクラムジェットモード試験

• Material Type: 規格・テクニカルリポート類
• Title: 複合エンジン燃焼器におけるスクラムジェットモード試験
• Author/Editor: 加藤, 周徳; 苅田, 丈士; 富岡, 定毅; 小林, 完; 工藤, 賢司; 村上, 淳郎; Kato, Kanenori; Kanda, Takeshi; Tomioka, Sadatake; Kobayashi, Kan; Kudo, Kenji; Murakami, Atsuo
• Author Heading: 加藤, 周徳; 苅田, 丈士; 富岡, 定毅; 小林, 完; 工藤, 賢司; 村上, 淳郎; Kato, Kanenori; Kanda, Takeshi; Tomioka, Sadatake; Kobayashi, Kan; Kudo, Kenji; Murakami, Atsuo
• Publication, Distribution, etc.: 宇宙航空研究開発機構
• Publication Date: 2006-01-20
• Publication Date (W3CDTF): 2006-01-20
• Alternative Title: Experimental study of combined cycle engine in scramjet-mode
• Periodical title: 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:宇宙輸送系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Space Transportation Systems
• No. or year of volume/issue: JAXA-SP-05-010
• Volume: JAXA-SP-05-010
• Pages: 69-74
• ISSN (Periodical Title): ISSN : 1349-113X
• Text Language Code: jpn
• Subject Heading: ロケットエンジン設計; 複合サイクルエンジン; 推薬燃焼; スクラムジェットエンジン; エンジン試験; ストレートダクト; 壁圧; 圧力分布; 燃焼効率; 当量比; rocket engine design; combined cycle engine; propellant combustion; scramjet engine; engine test; straight duct; wall pressure; pressure distribution; combustion efficiency; equivalence ratio
• Target Audience: 一般
• Note (General): 出版タイプ： NA; A rocket based combined cycle engine combustor was tested in scramjet-mode. The combustor model has two rockets in the combustor section. These rockets were used not only for thrust production, but also for fuel supply. The test facility consisted of an air supply section, a combustor section, a straight duct section, and a divergent duct section. Total pressure of the supplied air was 1 MPa, and the total temperature of the air was 2,400 K. In the tests, length of the straight duct section was changed to investigate its effects on the combustor performance. Two combustion patterns were observed for different lengths of straight duct. Pitot pressure and gas sampling were measured on the exit plane of the combustor model. Better combustion conditions were attained in the case of a longer duct.; 資料番号: AA0049056015; レポート番号: JAXA-SP-05-010
• Periodical Title (NCID): AA11984031; https://ci.nii.ac.jp/ncid/AA11984031
• Data Provider (Database): 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）; https://irdb.nii.ac.jp
• Original Data Provider (Database): 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