Výsledky vyhledávání - "デトネーション"

Autor: Tsuji, Toshiyuki, Shirakawa, Shinichi, Yoshihashi, Teruo, Obara, Tetsuro, Oyagi, Shigeharu

Publikováno v: 宇宙航空研究開発機構特別資料: 第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集 = JAXA Special Publication: Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007. :149-153

The two-cylinder Pulse Detonation Engine (PDE) with a single converging nozzle connected to an automotive turbocharger system was constructed. It was investigated to estimate the interference of pressure waves between two cylinders and to measure the

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::733f92813507acae16f78dbe2ba356b7
http://id.nii.ac.jp/1696/00005624/

Zobrazit plný text záznamu

Conditions for high efficiency flight of a pulse detonation engine

Autor: Furukawa, Takeshi, Fujiwara, Toshitaka

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :101-104

The performances of pulse detonation engine (PDE) were numerically estimated with detailed chemical reaction model. Flight altitude, flight Mach number, PDE-tube length and fuel-injection forms, i.e. equivalence ratio and distribution of equivalence

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6b74ad1e1709370af2dbce2284e4b2e0
http://id.nii.ac.jp/1696/00017250/

Zobrazit plný text záznamu

Pulse detonation system using flame jet ignition

Autor: Hayashi, Koichi, Sato, Hiroyuki, Kenmoku, Yasuhiro, Shimada, Hidetoshi

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :105-108

資料番号: AA0047118027

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::52596802070ccb95b83a98469cc34e1d
http://id.nii.ac.jp/1696/00017251/

Zobrazit plný text záznamu

Effect of a fuel injection scheme on the PDE propulsion performance

Autor: Furukawa, Takeshi, Fujiwara, Toshitaka

Publikováno v: 宇宙輸送シンポジウム平成14年度 = Proceedings of Space Transportation Symposium FY2002. :59-62

資料番号: AA0045426015

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::dd31930c6ce11bd82187ded3e39c219f
http://id.nii.ac.jp/1696/00017345/

Zobrazit plný text záznamu

Development of a pulse detonation engine at Aoyama Gakuin University

Autor: Sato, Hiroyuki, Kenmoku, Yasuhiro, Shimada, Hidetoshi, Fujii, Kunihide, Tsuboi, Nobuyuki, Hayashi, Koichi

Publikováno v: 宇宙輸送シンポジウム平成14年度 = Proceedings of Space Transportation Symposium FY2002. :63-66

資料番号: AA0045426016

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::6ebc884e64480f585f7a9f3c67405897
http://id.nii.ac.jp/1696/00017346/

Zobrazit plný text záznamu

Developmental research on PDE performance with DDT optimization

Autor: Zhang, Feng-Yuan, Nakayama, Eiichi, Hattori, Tsuyoshi, Yoshida, Satoru, Azuma, Nobuyuki, Fujiwara, Toshitaka, Miyasaka, Takeshi, Saito, Akira, Tamugi, Azusa

Publikováno v: 宇宙輸送シンポジウム平成13年度 = Proceedings of Space Transportation Symposium FY2001. :115-118

An experiment research on pulse detonation engine (PDE), which is developed in Nagoya University, is conducted with hydrogen/air. The fuel and oxidizer are injected into the tube with the opposite directions and are mixed by the collision of the two

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::92f1a5a722cb478c2ec5014d3a2d6a0d
http://id.nii.ac.jp/1696/00017451/

Zobrazit plný text záznamu

Vyhledávací nástroje:

Upřesnit hledání