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Shear and Swirl Coaxial Injector Studies of LOX/GCH4 Rocket Combustion Using Non- Intrusive Laser Diagnostics

机译：使用非侵入式激光诊断技术对LOX / GCH4火箭燃烧的剪切和旋流同轴喷油器研究

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《AIAA Aerospace Sciences Meeting and Exhibit》|2006年|P.1-14|共14页
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D. Salgues; A. Mouis; S. Lee; D. Kalitan; S. Pal; R. Santoro;
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中图分类航空;
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1. Combustion behaviors of GO2/GH2 swirl-coaxial injector using non-intrusive optical diagnostics [J] . Cai GuoBiao, Dai Jian, Zhang Yang, Acta astronautica . 2016,第junaajula期

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2. Investigation of non-premixed flame combustion characters in GO2/GH2 shear coaxial injectors using non-intrusive optical diagnostics [J] . DAI Jian, YU NanJia, CAI GuoBiao 中国科学:物理学力学天文学（英文版） . 2015,第012期

机译：使用非侵入式光学诊断研究GO2 / GH2剪切同轴注射器非预混合火焰燃烧特性
3. Study on the Design Criteria of the Coaxial Injector for a LOX/Hydrogen Rocket Engine: Evaluation of Design for Injectors of the LE-5 Engine and Its Derivatives [J] . Nobuyuki Yatsuyanagi Transactions of the Japan society for aeronautical and space sciences . 2007,第169期

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4. Shear and Swirl Coaxial Injector Studies of LOX/GCH4 Rocket Combustion Using Non- Intrusive Laser Diagnostics [C] . American Institute of Aeronautics and Astronautics Aerospace Sciences Meeting and Exhibit . 2006

机译：使用非侵入式激光诊断剪切和旋流同轴注射器研究LOX / GCH4火箭燃烧
5. Primary atomization study of a swirl coaxial liquid propellant rocket injector. [D] . Rahman, Shamim Aejaz. 1997

机译：涡旋同轴液体推进剂火箭喷射器的初步雾化研究。
6. New diagnostic methods for laser plasma- and microwave-enhanced combustion [O] . Richard B Miles, James B Michael, Christopher M Limbach, -1

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7. Numerical Investigation of Coaxial GCH4/LOx Combustion at Supercritical Pressures [O] . Sindhuja Priyadarshini, Malay K Das, Ashoke De, 2020

机译：超临界压力同轴GCH4 / LOX燃烧的数值研究
8. Design and Study of a LOX/GH2 Throttleable Swirl Injector for Rocket Applications [R] . Greene, Christopher, Woodward, Roger, Pal, Sibtosh, 2002

机译：用于火箭应用的LOX / GH2可调节涡流喷射器的设计与研究

Shear and Swirl Coaxial Injector Studies of LOX/GCH4 Rocket Combustion Using Non- Intrusive Laser Diagnostics

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