每年研究成果
每年研究成果
- 6結果
搜尋結果
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2023
Two-Stage Impinging-Jet Injector Flow Dynamics and Mixing: Kerosene and Hydrogen Peroxide Propellants
Chen, Y. T. & Yuan, T., 2023, (Accepted/In press) 於: Combustion science and technology. 196, 17, p. 4750-4767 18 p.研究成果: Article › 同行評審
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2018
The auto-ignition of kerosene-based sythetic fuel/hydrogen peroxide propellants and its injector design
Yuan, T., Chen, Y-T. & Zhou, J. Y., 2018 1月 1, 2018 Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-4775. (2018 Joint Propulsion Conference).研究成果: Conference contribution
2 引文 斯高帕斯（Scopus） -
2015
A cold-flow experimental observation of the two-stage impinging type injector for rocket propulsion
Huang, B., Yuan, T., Chen, Y. T. & Su, Y. H., 2015, 51st AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, (51st AIAA/SAE/ASEE Joint Propulsion Conference).研究成果: Conference contribution
1 引文 斯高帕斯（Scopus） -
Semi-hypergolic kerosene/hydrogen peroxide fuel system and its auto-ignition injector design
Yuan, T., Chen, Y. T., She, I. H. & Huang, B., 2015, 51st AIAA/SAE/ASEE Joint Propulsion Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, (51st AIAA/SAE/ASEE Joint Propulsion Conference).研究成果: Conference contribution
7 引文 斯高帕斯（Scopus） -
Spray characteristics of the high rotating speed slinger with different orifice diameter
Chen, Y. T., Huang, S. C., Lai, W. H. & Hong, C. H., 2015.研究成果: Paper › 同行評審
1 引文 斯高帕斯（Scopus） -
2012
The impinging-type injector design of MMH/NTO liquid rocket engine
Yuan, T., Chen, C., Huang, B., Tang, M. & Chen, Y. T., 2012, 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012. American Institute of Aeronautics and Astronautics Inc., (48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012).研究成果: Conference contribution
2 引文 斯高帕斯（Scopus）