Zobrazeno 1 - 10 of 50 pro vyhledávání: '"Atsuo MURAKAMI"'
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Akademický článek
Estimation of Mode Transition in a Supersonic Combustor
Autor: Junji NODA, Atsuo MURAKAMI, Kenji KUDO, Sadatake TOMIOKA
Publikováno v: Journal of Thermal Science and Technology, Vol 8, Iss 2, Pp 353-362 (2013)
A quasi-one dimensional calculation was carried out to figure out supersonic combustor performances. Three flow tubes were considered in the combustor region. Those were an air-flow-tube, a combustion-flow-tube and a fuel-flow-tube. A Mach=1 conditio
Externí odkaz: https://doaj.org/article/10ab712b0bd04002bb16470744f5a121
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2
An Experimental Investigation on Combustion Characteristics of Hypermixer Injectors–Effects of the ‘Swept’ Applied to Hypermixer Injector Ramps
Autor: Noritsugu Kubo, Sadatake Tomioka, Kenji Kudo, Atsuo Murakami
Publikováno v: Procedia Engineering. 99:954-960
Supersonic mixing and combustion enhancement is the key technology for success of the development of the scramjet engine. In this study, some types of hypermixer (ramp) injectors were investigated by the combustion test. Especially, we have focused o
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ee640723c0afcc00529555989b7c1f42
https://doi.org/10.1016/j.proeng.2014.12.627
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4
Experimental Study on Combustion Modes in a Supersonic Combustor
Autor: Kanenori Kato, Ryou Masumoto, Kenji Kudo, Atsuo Murakami, Hiroyuki Yamasaki, Sadatake Tomioka
Publikováno v: Journal of Propulsion and Power. 27:346-355
obliquefuelinjectionwasemployedtomitigatefueljet/airflowinteraction,theinteractionwasfoundtohaveasizable effect on the ignition limit. A simple model to predict the minimum combustor length needed to attain supersonic or dual-mode combustion was sugg
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::8af58fe0716e20cc016d3d3665bb55e0
https://doi.org/10.2514/1.b34020
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6
Performance of a Dual-Mode Combustor with Multistaged Fuel Injection
Autor: Kanenori Kato, Kan Kobayashi, Kenji Kudo, Atsuo Murakami, Sadatake Tomioka
Publikováno v: Journal of Propulsion and Power. 22(3):518-526
A scramjet combustor, which has a constant cross-sectional area combustor (designated as combustor 1), and a diverging combustor (designated as combustor 2), was examined with both single and two-stage fuel injection to determine whether it could be
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ad4b44fa25cdc27bb248eb67b0f2e3c9
http://id.nii.ac.jp/1696/00021467/
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Distributed Fuel Injection for Performance Improvement of Staged Supersonic Combustor
Autor: Sadatake Tomioka, Atsuo Murakami, Kenji Kudo, Kan Kobayashi
Publikováno v: Journal of Propulsion and Power. 21:760-763
Introduction S UBSCALE model scramjet engines have been tested at Japan Aerospace Exploration Agency—Kakuda Space Propulsion Center (formerly National Aerospace Laboratory—Kakuda Space Propulsion Laboratory).1 The models consisted of a sidecompre
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::74cd9fa94153e3110a4bf9f5cbe997ae
https://doi.org/10.2514/1.6172
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