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| Advances in Plasma Diagnostics and Applications 专著
Beijing:MDPI, 2022
作者: Editors：Chen ZT; Attri P; Wang Q(汪球)
 Adobe PDF(20682Kb) |  收藏 | 浏览/下载：407/1 | 提交时间：2022/12/03 |
| Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
作者: Jiang ZL(姜宗林) ; Teng, Honghui
Adobe PDF(13641Kb) | 收藏 | 浏览/下载：104/2 | 提交时间：2023/03/23 |
| Formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
作者: Zhang ZJ(张子健); Wen, Chihyung; Zhang WS(张文硕); Liu YF(刘云峰); Jiang ZL(姜宗林)
 Adobe PDF(3599Kb) | 收藏 | 浏览/下载：325/88 | 提交时间：2021/03/03
Oblique detonation wave Combustor Oblique detonation engine Normal detonation wave Boundary layer separation |
| 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
作者: Li B(李波); Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(1358Kb) | 收藏 | 浏览/下载：150/45 | 提交时间：2021/02/01 |
| Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
作者: Yao W(姚卫)
 浏览 | Adobe PDF(9586Kb) | 收藏 | 浏览/下载：643/293 | 提交时间：2019/12/17
Kerosene Supersonic combustion Large eddy simulation Skeletal mechanism Scramjet |
| Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
作者: Meng Y(孟宇); Gu HB(顾洪斌); Zhuang JH(庄金衡); Sun WM(孙文明); Gao ZB(高占彪); Lian H(连欢); Yue LJ(岳连捷); Chang XY(张新宇)
浏览 | Adobe PDF(3099Kb) | 收藏 | 浏览/下载：361/94 | 提交时间：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| Influences of Domain Symmetry on Supersonic Combustion Modeling 期刊论文
JOURNAL OF PROPULSION AND POWER, 2019, 卷号: 35, 期号: 2, 页码: 451-465
作者: Yao W(姚卫); Wu K(吴坤); Fan XJ(范学军)
Adobe PDF(862Kb) | 收藏 | 浏览/下载：320/97 | 提交时间：2019/04/11 |
| Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(623Kb) | 收藏 | 浏览/下载：258/87 | 提交时间：2018/01/16
Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者: Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(832Kb) | 收藏 | 浏览/下载：271/81 | 提交时间：2018/11/08
Combustion Cost benefit analysis Costs Mixtures Ramjet engines Supersonic aircraft Computational costs Equivalence ratios Local flow conditions Scramjet combustors Statistics approaches Supersonic combustion Supersonic combustors Turbulent combustion |
| Detailed transitional process of the flames in hot and diluted environments from lifted flames to MILD combustion 会议论文
10th U.S. National Combustion Meeting, College Park, MD, United states, April 23, 2017 - April 26, 2017
作者: Liu CY; Zhang J(张健)
Adobe PDF(414Kb) | 收藏 | 浏览/下载：216/76 | 提交时间：2018/11/08
Oxygen Diluted environments Monotonic trend Partial premixing Stabilization mechanisms Transition process Transitional flames Transitional process Turbulent combustion |
