Zobrazeno 1 - 10
of 23
pro vyhledávání: '"Tetsuji Sunami"'
Autor:
Masaki Mitani, Atsunari Hiraya, Keiichiro Waki, Hiroaki Yoshida, Fumitaka Tahara, Yasunori Senba, Tetsuji Sunami, Ko Saito, Lars G. M. Pettersson, Osamu Takahashi
Publikováno v:
Journal of Electron Spectroscopy and Related Phenomena. 142(2):113-119
Density functional theory (DFT) has been applied to simulate core-excited photoabsorption spectra for some methylcyano esters within a transition potential (TP) framework. Our calculations for methylcyano formate at the N and O K-edges are consistent
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 53:467-481
A scramjet engine with a wall-mounted hypermixer injector, which generates streamwise vortices for enhancing supersonic mixing and combustion, is examined at a Mach 8 simulated flight condition in the High Enthalpy Shock Tunnel (HIEST). The engine an
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 50:22-29
Publikováno v:
Journal of Propulsion and Power. 18(2):417-423
著者人数: 5名
資料番号: AC1000025000
資料番号: AC1000025000
Publikováno v:
Journal of Propulsion and Power. 17:617-621
Combustion tests of a scramjet engine were conducted to obtain thrust, lift, and pitching moment essential for evaluation of the engine’s basic performance and for determination of the requirements to control the system of integrated engine and bod
Publikováno v:
Journal of Propulsion and Power. 17:132-138
著者人数: 5名
資料番号: AC1000022000
資料番号: AC1000022000
Autor:
Kouichiro Tani, Muneo Izumikawa, Tetsuji Sunami, Toshihito Saito, Nobuo Chinzei, Takashi Shimura
Publikováno v:
Journal of the Japan Society for Aeronautical and Space Sciences. 44:623-628
Autor:
Tetsuji Sunami, Masatoshi Kodera
Publikováno v:
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference.
Autor:
Toshihiko Hiejima, Takakage Arai, Michio Nishioka, Shoji Sakaue, Tetsuji Sunami, Hiroki Hayase
Publikováno v:
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
For supersonic mixing enhancement, large scale streamwise vortices seem to be the most advantageous. In SCRAM jet (supersonic combustion ramjet) engine, the device which introduces both the large scale streamwise vortices and fuel into supersonic flo
Publikováno v:
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference.
A hydrogen fueled scramjet engine with a wall-mounted hypermixer injector is examined at a Mach 8 flight condition in the high enthalpy shock tunnel. The hypermixer, which is previously proposed by JAXA for the use over a wide range of flight Mach nu