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A design methodology for rapid implementation of active control systems across lean direct injection combustor platforms [microform] / William T. Baumann, William R. Saunders, and Uri Vandsburger (NASA/CR-2003-212197)

A design methodology for rapid implementation of active control systems across lean direct injection combustor platforms [microform] / William T. Baumann, William R. Saunders, and Uri Vandsburger (NASA/CR-2003-212197)
マイクロ図書
2003<YCA-NAS 1.26:212197>
国立国会図書館
  • 件名Active control Combustion control Injectors Fuel injection Combustion ch...

Experimental evaluation of a subscale gaseous hydrogen/gaseous oxygen coaxial rocket injector [microform] / Timothy D. Smith ... [et al.] (NASA/TM-2002-211982)

Experimental evaluation of a subscale gaseous hydrogen/gaseous oxygen coaxial rocket injector [microform] / Timothy D. Smith ... [et al.] (NASA/TM-2002-211982)
マイクロ図書
2002<YCA-NAS 1.15:2002-211982>
国立国会図書館
  • 件名Rocket engines Injectors Gaseous rocket propellants R...

Development of anti-coking thermal management technologies for a coaxially-staged lean-burn fuel injector for high-pressure-ratio aero-engines.: First report: Evaluation of thermal protection performance and validation of numerical analysis by experiments in realistic environments.

Development of anti-coking thermal management technologies for a coaxially-staged lean-burn fuel injector for high-pressure-ratio aero-engines.: First report: Evaluation of thermal protection performance and validation of numerical analysis by experiments in realistic environments.
デジタル規格・テクニカルリポート類
松浦, 一哲, 山本, 武Japan Aerospace Exploration Agency (JAXA)2025-02-27JAXA Research and Development MemorandumJAXA-RM-24-008E
インターネットで読める全国の図書館
  • 件名Fuel injector design Lean staged combustor Injector thermal management Fuel cokin...
  • 一般注記...lean-burn fuel injector for aero-engin......shown that the injector of the current...... evaluation of injector performance. I......esults for the injector with one of su...... design of the injector and its manufacturing process...

Analysis and modeling of a two-phase jet pump of a thermal management system for aerospace applications [microform] / S.A. Sherif ... [et al.] ([NASA contractor report] ; NASA/CR-208243)

Analysis and modeling of a two-phase jet pump of a thermal management system for aerospace applications [microform] / S.A. Sherif ... [et al.] ([NASA contractor report] ; NASA/CR-208243)
マイクロ図書
1998<YCA-NAS 1.26:208243>
国立国会図書館
  • 件名Jet pumps Injectors Temperature control Throats ...

低毒性イオン液体推進剤の微粒化特性に関する実験的研究

低毒性イオン液体推進剤の微粒化特性に関する実験的研究
デジタル規格・テクニカルリポート類
伊藤, 尚義, 黒田, 彬斗, 尾松, 来基, 半澤, 佳祐, 勝身, 俊之, 門脇, 敏, ITO, Hisayoshi, KURODA, Yoshito, OMATSU, Raiki, HANZAWA, Keisuke, KATSUMI, Toshiyuki, KADOWAKI, Satoshi宇宙航空研究開発機構(JAXA)2023-02-03宇宙航空研究開発機構研究開発報告: 高エネルギー物質研究会: 令和4年度研究成果報告書 = JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2022)JAXA-RR-22-006p.25-28
全国の図書館
  • 件名Hydroxyl Ammonium Nitrate Ammonium Dinitramide Atomization Swirl injector
  • 一般注記...ant by a swirl injector. According to the previous st...

Development of a device to deploy fluid droplets in microgravity [microform] / David W. Robinson and An-Ti Chai (NASA TM ; 107460)

Development of a device to deploy fluid droplets in microgravity [microform] / David W. Robinson and An-Ti Chai (NASA TM ; 107460)
マイクロ図書
1997<YCA-NAS 1.15:107460>
国立国会図書館
  • 件名Microgravity Drops (Liquids) Bubbles Injectors Heat transfer Dispensers

Injector mixing efficiency experiments [microform] : final report : contract number NAS8-38609 D.O. 159 / prepared by Marlow D. Moser, principal investigator

Injector mixing efficiency experiments [microform] : final report : contract number NAS8-38609 D.O. 159 / prepared by Marlow D. Moser, principal investigator
マイクロ図書
1998<YCA-NAS 1.26:208190>
国立国会図書館
  • 件名Experimentation Injectors Combustion chambers Controll...

Effects of jet swirl on mixing of a light gas jet in a supersonic airstream [microform] / Steven E. Doerner and Andrew D. Cutler ([NASA contractor report] ; NASA CR-1999-209842)

Effects of jet swirl on mixing of a light gas jet in a supersonic airstream [microform] / Steven E. Doerner and Andrew D. Cutler ([NASA contractor report] ; NASA CR-1999-209842)
マイクロ図書
1999<YCA-NAS 1.26:209842>
国立国会図書館
  • 件名...rling Gas jets Injectors Turbulent mixing Fuel system...

Ammonium Dinitramide系低毒性推進剤の微粒化特性改善手法の検討

Ammonium Dinitramide系低毒性推進剤の微粒化特性改善手法の検討
デジタル規格・テクニカルリポート類
伊藤, 尚義, 尾松, 来基, 半澤, 佳祐, 勝身, 俊之, 門脇, 敏, ITO, Hisayoshi, OMATSU, Raiki, HANZAWA, Keisuke, KATSUMI, Toshiyuki, KADOWAKI, Satoshi宇宙航空研究開発機構(JAXA)2021-02-10宇宙航空研究開発機構研究開発報告: 高エネルギー物質研究会: 令和2年度研究成果報告書 = JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2020)JAXA-RR-20-007p.5-8
全国の図書館
  • 件名Ammonium Dinitramide Monopropellant Thruster Injector Atomization

On the roles of spray response to pressure oscillations in combustion instability in a combustor with a lean-burn coaxially-staged fuel injector for aero-engines.: First report: Preliminary attempts on fuel flow rate response.

On the roles of spray response to pressure oscillations in combustion instability in a combustor with a lean-burn coaxially-staged fuel injector for aero-engines.: First report: Preliminary attempts on fuel flow rate response.
デジタル規格・テクニカルリポート類
松浦, 一哲, 加藤, 昂大, 佐々木, 悠太, 座間, 淑夫, 山本, 武, 黒瀬, 良一Japan Aerospace Exploration Agency (JAXA)2025-02-26JAXA Research and Development MemorandumJAXA-RM-24-003E
インターネットで読める全国の図書館
  • 件名Combustion instability Spray response Aero-engine Lean-burn fuel injector Large eddy simulation
  • 一般注記...ly-staged fuel injector for aero-engin......ressure of the injector were modulated by a siren. Th...

An experimental study of characteristic combustion-driven flow for CFD validation [microform] : final report for NASA contract NAS8-38862 / by Robert J. Santoro ([NASA contractor report] ; 205735)

An experimental study of characteristic combustion-driven flow for CFD validation [microform] : final report for NASA contract NAS8-38862 / by Robert J. Santoro ([NASA contractor report] ; 205735)
マイクロ図書
1997<YCA-NAS 1.26:208258>
国立国会図書館
  • 件名...ty measurement Injectors Combustible flow

Development of tripropellant CFD design code [microform] : contract no.--NAS8-40583 : final report / prepared by Richard C. Farmer, Gary C. Cheng, Peter G. Anderson

Development of tripropellant CFD design code [microform] : contract no.--NAS8-40583 : final report / prepared by Richard C. Farmer, Gary C. Cheng, Peter G. Anderson
マイクロ図書
1998<YCA-NAS 1.26:207893>
国立国会図書館
  • 件名...Rocket engines Injectors Flow distribution Combustion

Dual Injector を用いたCBCTの検討

Dual Injector を用いたCBCTの検討
デジタル規格・テクニカルリポート類
柏木, 正人, 増島, 一貴, 荒井, 一正, 川原, 明世日本赤十字社医学会2018-09-01日赤医学70 1p.267-267
全国の図書館
  • 件名CBCT TACE Dual Injector

Space transportation booster engine thrust chamber technology [microform] : final report / prepared by J.A. Schneider ([NASA contractor report] ; NASA CR-192531)

Space transportation booster engine thrust chamber technology [microform] : final report / prepared by J.A. Schneider ([NASA contractor report] ; NASA CR-192531)
マイクロ図書
1993<YCA-NAS 1.26:192531>
国立国会図書館
  • 件名Space shuttles -- Propulsion systems Injectors

Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept [microform] / M.M. Fazah and J.M. Cramer (NASA/TM ; 1998-208194)

Thruster injector faceplate testing in support of the aerojet Rocket-based combined cycle (RBCC) concept [microform] / M.M. Fazah and J.M. Cramer (NASA/TM ; 1998-208194)
マイクロ図書
1998<YCA-NAS 1.15:208194>
国立国会図書館
  • 件名Injectors Gas-gas interactions Rocket ...

Evaluation of a training program on initial actions against anaphylaxis in children with food allergies in nursery schools

Evaluation of a training program on initial actions against anaphylaxis in children with food allergies in nursery schools
デジタル博士論文
阿久澤, 智恵子群馬大学大学院保健学研究科2019-03-22
インターネットで読める全国の図書館
  • 件名adrenaline auto—injector anaphylactic shock food aller...

Flow distribution around the SSME main injector assembly using porosity formulation [microform] / Gary C. Cheng, Yen-Sen Chen, and Ten-See Wang ([NASA contractor report] ; NASA-CR-202070)

Flow distribution around the SSME main injector assembly using porosity formulation [microform] / Gary C. Cheng, Yen-Sen Chen, and Ten-See Wang ([NASA contractor report] ; NASA-CR-202070)
マイクロ図書
1995<YCA-NAS 1.26:202053>
国立国会図書館
  • 件名...le main engine Injectors Porosity Turbulent flow High...

Steam-injection pressing of isocyanate-bonded aspen flakeboards : latitudes and limitations / Robert L. Geimer (Research paper FPL ; 456)

Steam-injection pressing of isocyanate-bonded aspen flakeboards : latitudes and limitations / Robert L. Geimer (Research paper FPL ; 456)
マイクロ図書
1985<YCA-A 13.78:FPL-456>
国立国会図書館
  • 件名Particle board Steam, High-pressure Injectors Steam engineering

Operator, organizational, direct support, and general support maintenance manual including repair parts list for test set, injector (Bacharach Instrument Company) (4910-00-355-6248), model YHQ [microform] (Department of the Army technical manual ; TM 9-4910-611-14 & P)

Operator, organizational, direct support, and general support maintenance manual including repair parts list for test set, injector (Bacharach Instrument Company) (4910-00-355-6248), model YHQ [microform] (Department of the Army technical manual ; TM 9-4910-611-14 & P)
マイクロ図書
1995<YCA-D 101.11:9-4910-611-14&P>
国立国会図書館
  • 件名Injectors -- United States -- Testing ...
  • 並列タイトル等（連結）Test set, injector (Bacharach Instrument Company...
  • 並列タイトル等Test set, injector (Bacharach Instrument Company...

液膜式気流噴射弁の設計パラメータ・作動条件が噴霧特性に与える影響: 第二報 気流・液膜の旋回及び噴射弁出口形状の影響

液膜式気流噴射弁の設計パラメータ・作動条件が噴霧特性に与える影響: 第二報 気流・液膜の旋回及び噴射弁出口形状の影響
デジタル規格・テクニカルリポート類
鈴木, 俊介, 須田, 充, 松浦, 一哲, 林, 茂, Suzuki, Syunsuke, Suda, Mitsuru, Matsuura, Kazuaki, Hayashi, Shigeru宇宙航空研究開発機構2009-02-27宇宙航空研究開発機構研究開発資料 = JAXA Research and Development MemorandumJAXA-RM-08-015
全国の図書館
  • 件名Aero Engine Fuel Injector Design, Fuel Atomization, Spr...
  • 一般注記...ro-engine fuel injectors. This second report discusse...
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