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Numerical Investigation on CO Emissions in Lean Premixed Combustion

Numerical Investigation on CO Emissions in Lean Premixed Combustion
Digital博士論文障害者向け資料あり
Yunoki, Keita2022-03-23
Available onlineNational Diet LibraryOther Libraries in Japan
  • Subject HeadingLean premixed combustion Carbon monoxide Heat loss Gas turbine combustor Flamelet approaches

Measurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors [microform] / Andreja Brankovic ... [et al.] (NASA/TM-2002-211127)

Measurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors [microform] / Andreja Brankovic ... [et al.] (NASA/TM-2002-211127)
Microform図書
2002<YCA-NAS 1.15:2002-211127>
National Diet Library
  • Subject HeadingCombustor Lobe mixer Supersonic flow Pi...

Effect of Jet Strength on NOx Formation in Premixed Impinging Jet Combustion with Minimum Heat Losses

Effect of Jet Strength on NOx Formation in Premixed Impinging Jet Combustion with Minimum Heat Losses
Digital文書・図像類
林, 茂, XIE, Lin, HAYASHI, Shigeru航空宇宙技術研究所1994-06航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-1237T1237Tp.8-
Other Libraries in Japan
  • Subject HeadingNOx formation; impinging jet combustion in a ceramic combustor; heat losses
  • Note (General)... impinging jet combustor with minimum h......oadings of the combustor ranged from 1.......of mixture per combustor volume. Impingement of jets o...

Characteristics of Heat Transfer to Nickel Plated Chamber Walls of High Pressure Rocket Combustors

Characteristics of Heat Transfer to Nickel Plated Chamber Walls of High Pressure Rocket Combustors
Digital文書・図像類
KUMAKAWA, Akinaga, SASAKI, Masaki, SATO, Kazuo, ONO, Fumiei, SAKAMOTO, Hiroshi, YATSUYANAGI, Nobuyuki航空宇宙技術研究所1991-10航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-1126T1126Tp.15-
Other Libraries in Japan
  • Subject Headingheat transfer; rocket combustor; nickel plating; thermal re...
  • Note (General)...d calorimetric combustors of different chamber length ...

小型風洞とエンジン補完実験

小型風洞とエンジン補完実験
Digital文書・図像類
三谷, 徹, 平岩, 徹夫, 苅田, 丈士, 志村, 隆, 富岡, 定毅, 小林, 完, 泉川, 宗男, 櫻中, 登, 渡邊, 修一, 樽川, 雄一, Mitani, Toru, Hiraiwa, Tetsuo, Kanda, Takeshi, Shimura, Takashi, Tomioka, Sadatake, Kobayashi, Kan, Izumikawa, Muneo, Sakuranaka, Noboru, Watanabe, Shuichi, Tarukawa, Yuichi航空宇宙技術研究所2003-04航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1458
Other Libraries in Japan
  • Subject Heading...al measurement combustor Mach number research and deve...
  • Note (General)...d. A series of combustor experiments us......ps in scramjet combustors. In the component experiment...

航技研におけるガスタービンおよびジェットエンジン燃焼器研究開発

航技研におけるガスタービンおよびジェットエンジン燃焼器研究開発
Digital文書・図像類
田丸, 卓, Tamaru, Takashi航空宇宙技術研究所1995-01航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory676p.1-113
Other Libraries in Japan
  • Subject Heading...ine jet engine combustor research and d......ure combustion combustor form combustor performance test engine inlet...
  • Note (General)...of gas turbine combustors are described...... placed on the combustor development fo......he gas turbine combustors are also described. 資料番号: AA...
  • Alternative TitleResearch and development of combustors for gas turbine and jet engi...

PLIFによる燃焼場でのOH濃度・温度分布計測

PLIFによる燃焼場でのOH濃度・温度分布計測
Digital文書・図像類
崎山, 幸紀, 黒澤, 要治, 五味, 光男, 鈴木, 和雄, Sakiyama, Yukinori, Kurosawa, Yoji, Gomi, Mitsuo, Suzuki, Kazuo航空宇宙技術研究所1999-11航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1394p.1-18
Other Libraries in Japan
  • Subject Heading...jet engine ram combustor ram flameholder burning flowf...

ラムジェットエンジン燃焼器用燃料内部冷却形保炎器の特性

ラムジェットエンジン燃焼器用燃料内部冷却形保炎器の特性
Digital文書・図像類
黒澤, 要治, 山本, 武, 斉藤, 隆, 田丸, 卓, Kurosawa, Yoji, Yamamoto, Takeshi, Saito, Takashi, Tamaru, Suguru航空宇宙技術研究所1999-05航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1384p.1-22
Other Libraries in Japan
  • Subject Heading... ramjet engine combustor fuel cooled flameholder hydro...
  • Note (General)... ramjet engine combustor for the space ......w-off when the combustor inlet velocity was increased ...
  • Alternative TitleExperimental investigation of a fuel-cooled flameholder for a ramjet engine combustor

燃料噴出型保炎器周りの流れに関する数値シミュレーションコードの開発

燃料噴出型保炎器周りの流れに関する数値シミュレーションコードの開発
Digital文書・図像類
山本, 武, 田丸, 卓, Yamamoto, Takeshi, Tamaru, Takashi航空宇宙技術研究所1994-04航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1233p.1-17
Other Libraries in Japan
  • Subject Heading...存 乱流消散火炎 CFD解析 combustor flow analysis ......pulsion ramjet combustor flow numerical flow simulatio...

Spray and combustion characteristics of a liquid-fueled ramjet combustor

Spray and combustion characteristics of a liquid-fueled ramjet combustor
Digital文書・図像類
佐々木, 正樹, 高橋, 守, 坂本, 博, 熊川, 彰長, 八柳, 信之, 清, 幹広, 吉村, 和彦, 稲村, 隆夫, Sasaki, Masaki, Takahashi, Mamoru, Sakamoto, Hiroshi, Kumakawa, Akinaga, Yatsuyanagi, Nobuyuki, Sei, Motohiro, Yoshimura, Kazuhiko, Inamura, Takao航空宇宙技術研究所1998-07航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1349Tp.1-16
Other Libraries in Japan
  • Subject Heading...ネトレーション ramjet combustor ramjet engine rocket ramjet e...
  • Note (General)... fueled ramjet combustor were experimen...... center of the combustor for flame hold...... center of the combustor; this region w......section of the combustor except in the ......ng of a ramjet combustor, was smaller than that of low...

ZrO2/Ni系完全傾斜機能型燃焼器の高空性能試験

ZrO2/Ni系完全傾斜機能型燃焼器の高空性能試験
Digital文書・図像類
黒田, 行郎, 佐藤, 政裕, 只野, 真, 森谷, 信一, 日下, 和夫, 熊谷, 達夫, 毛呂, 明夫, 田口, 秀之, 川又, 善博, 三木, 陽一郎, Kuroda, Yukio, Sato, Masahiro, Tadano, Makoto, Moriya, Shinichi, Kusaka, Kazuo, Kumagai, Tatsuo, Moro, Akio, Taguchi, Hideyuki, Kawamata, Yoshihiro, Miki, Yoichiro航空宇宙技術研究所1997-05航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1327p.1-18
Other Libraries in Japan
  • Subject Heading...ly graded type combustor ZrO2 Ni FGM combustion chambe...

矩形断面スクラムジェット燃焼器の実験　2:噴射部形状の影響

矩形断面スクラムジェット燃焼器の実験　2:噴射部形状の影響
Digital文書・図像類
村上, 淳郎, 小室, 智幸, 工藤, 賢司, Murakami, Atsuo, Komuro, Tomoyuki, Kudo, kenji航空宇宙技術研究所1993-12航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1220p.1-25
Other Libraries in Japan
  • Subject Heading...界層 保炎器 圧力分布 壁面 combustor scramjet rectangular cross se...
  • Note (General)...ction scramjet combustor was carried out. The effects ...
  • Alternative Title...ction scramjet combustor. Part 2: Effects of fuel inje...

ロケット-ラム複合燃焼器の実験

ロケット-ラム複合燃焼器の実験
Digital文書・図像類
佐藤, 和雄, 坂本, 博, 佐々木, 正樹, 小野, 文衛, 八柳, 信之, Sato, Kazuo, Sakamoto, Hiroshi, Sasaki, Masaki, Ono, Fumiei, Yatsuyanagi, Nobuyuki航空宇宙技術研究所1994-10航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1249p.1-17
Other Libraries in Japan
  • Subject Heading...t ram combined combustor propulsion double nozzle sing...
  • Note (General)...t-ram combined combustor with a total thrust of 5kN wa...
  • Alternative TitleExperiment of rocket-ram combined combustor

再生冷却式燃焼器用ZrO2/Ni系遮熱コーティング材料のNTO/MMH燃焼ガス加熱場におけるレーザー改質効果

再生冷却式燃焼器用ZrO2/Ni系遮熱コーティング材料のNTO/MMH燃焼ガス加熱場におけるレーザー改質効果
Digital文書・図像類
黒田, 行郎, 森谷, 信一, 只野, 真, 佐藤, 政裕, 毛呂, 明夫, 青木, 由雄, 須藤, 孝幸, 結城, 正弘, 下田, 信之, Zhang, Qing Jie, Kuroda, Yukio, Moriya, Shinichi, Tadano, Makoto, Sato, Masahiro, Moro, Akio, Aoki, Yoshio, Sudo, Takayuki, Yuki, Masahiro, Shimoda, Nobuyuki航空宇宙技術研究所1997-12航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1339p.1-28
Other Libraries in Japan
  • Subject Heading... cooled thrust combustor thermal barrier coating funct...

A computer model for the simulation of turbulent reacting flow in a jet assisted ram combustor

A computer model for the simulation of turbulent reacting flow in a jet assisted ram combustor
Digital文書・図像類
Kumar, S., Kumar, Sanjiv航空宇宙技術研究所1995-05航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1267Tp.1-22
Other Libraries in Japan
  • Subject Heading...combustion RAM combustor jet stabilized flame computer...
  • Note (General)...t assisted ram combustor is developed. Favre averaged ...

C/C複合材のロケット燃焼器への適用　その1:C/C複合材のロケット燃焼ガス加熱評価試験

C/C複合材のロケット燃焼器への適用　その1:C/C複合材のロケット燃焼ガス加熱評価試験
Digital文書・図像類
只野, 真, 佐藤, 政裕, 黒田, 行郎, 日下, 和夫, 植田, 修一, 末光, 毅, 長谷川, 聰, 久手, 幸徳, Tadano, Makoto, Sato, Masahiro, Kuroda, Yukio, Kusaka, Kazuo, Ueda, Shuichi, Suemitsu, Takeshi, Hasegawa, Satoshi, Kude, Yukinori航空宇宙技術研究所1995-04航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1264p.1-15
Other Libraries in Japan
  • Subject Heading...matrix coating combustor rocket engine heating test hi...

デュアル混合比液酸/水素燃焼器の燃焼・熱負荷特性　1

デュアル混合比液酸/水素燃焼器の燃焼・熱負荷特性　1
Digital文書・図像類
坂本, 博, 佐々木, 正樹, 高橋, 守, 佐藤, 和雄, 田村, 洋, Sakamoto, Hiroshi, Sasaki, Masaki, Takahashi, Mamoru, Sato, Kazuo, Tamura, Hiroshi航空宇宙技術研究所1995-09航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1278p.1-15
Other Libraries in Japan
  • Subject Heading...xygen/hydrogen combustor heat transfer characteristic ...
  • Note (General)...o LOX-hydrogen combustors. Experiments ......single-element combustors. The combustion test results...

A computer model in general 3-D curvilinear coordinates for the prediction of the turbulent flow field in a jet induced ram combustor

A computer model in general 3-D curvilinear coordinates for the prediction of the turbulent flow field in a jet induced ram combustor
Digital文書・図像類
Kumar, S., Kumar, Sanjiv航空宇宙技術研究所1994-06航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1240Tp.1-18
Other Libraries in Japan
  • Subject Heading...flow field ram combustor computer model three dimensio...
  • Note (General)...et induced ram combustor is developed. ......w field in the combustor. Computed results showing the...

スクラムジェットにおける化学反応:簡略化反応系による考察

スクラムジェットにおける化学反応:簡略化反応系による考察
Digital文書・図像類
三谷, 徹, Mitani, Toru航空宇宙技術研究所1992-11航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1184p.1-29
Other Libraries in Japan
  • Subject Heading...ngine scramjet combustor chemically reacting flow reac...
  • Note (General)... combustion in combustors and reactive ......ng in scramjet combustors are discussed using the mode...

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