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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) Adobe PDF(1358Kb)  |  Favorite  |  View/Download:177/59  |  Submit date:2021/02/01 |
| 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 Adobe PDF(1785Kb)  |  Favorite  |  View/Download:147/58  |  Submit date:2021/02/01 |
| Numerical simulation of 30p30n multi-element airfoil using delayed detached-eddy simulation 会议论文 AIAA AVIATION 2020 FORUM, 15 June 2020 through 19 June 2020 Authors: Jin Y; 廖飞, Cai JS Adobe PDF(4611Kb)  |  Favorite  |  View/Download:244/123  |  Submit date:2021/06/11 |
| 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) Adobe PDF(2272Kb)  |  Favorite  |  View/Download:297/153  |  Submit date:2021/06/11 |
| A method for rapid generation of 3D infrared radiation intensity field of engine exhaust plume 会议论文 6th Symposium on Novel Optoelectronic Detection Technology and Applications, Beijing, PEOPLES R CHINA, 3 December 2019 through 5 December 2019 Authors: Bao XD(包醒东); Yu XL(余西龙); Wang Z.-H; Mao H.-X; Xiao Z.-H. Adobe PDF(602Kb)  |  Favorite  |  View/Download:187/80  |  Submit date:2021/06/11 Calculation method Exhaust plume Infrared spectroscopy Radiation intensity Three-dimensional space |
| 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) Adobe PDF(1569Kb)  |  Favorite  |  View/Download:234/69  |  Submit date:2021/06/11 concentration hybrid rocket motor nozzle exit temperature Tunable diode laser absorption spectroscopy (TDLAS) water vapor |