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| Plasma properties measurements of parallel-plane electrodes in Argon by coupling OES and PLIF 会议论文 Global Intelligent Industry Conference, 中国上海, 2020/10/28-30 Authors: Wang FY(王方仪); Zhang SH(张少华) ; Yu XL(余西龙)![](/image/person.jpg)
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| Evaluation of the influence of radiation on a GH2/GO2 rocket combustor 会议论文 AIAA Propulsion & Energy Forum, VIRTUAL EVENT, 2020-08-17 Authors: Li B(李波); Yao W(姚卫) ; Fan XJ(范学军)![](/image/person.jpg)
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| Numerical simulation of acoustic scattering and flow-induced noise with sharp interface immersed boundary method 会议论文 AIAA Scitech 2020 Forum, Orlando, FL, 2020/1/6-10 Authors: Zhao C; Yang Y(杨焱) ; Zhang T; Dong HB
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| Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model 会议论文 AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020 Authors: Yao W(姚卫) ; Chen L(陈留)
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| Temperature and H2O concentration measurements for a hybrid rocket motor plume using a single mid-infrared tunable diode laser 会议论文 2020 Applied Optics and Photonics China: Optical Sensing and Imaging Technology, AOPC 2020, Xiamen, PEOPLES R CHINA, 25 August 2020 through 27 August 2020 Authors: Fang SH(方思晗); Wang ZZ(王泽众) ; Li RJ(李仁杰) ; Zhang ZL(张泽林); Lin X(林鑫) ; Li F(李飞) ; Yu XL(余西龙)![](/image/person.jpg)
Adobe PDF(1569Kb)  |   Favorite  |  View/Download:233/69  |  Submit date:2021/06/11 concentration hybrid rocket motor nozzle exit temperature Tunable diode laser absorption spectroscopy (TDLAS) water vapor |