机构

• 力学研究所 [10]

采集方式

• OAI收割 [10]

内容类型

• 期刊论文 [10]

发表日期

• 2023 [1]
• 2022 [3]
• 2019 [1]
• 2018 [1]
• 2015 [1]
• 2012 [2]
• 更多

学科主题

• 流体力学::实验流体... [2]
• 固体力学::弹性力学... [1]

筛选

浏览/检索结果: 共10条，第1-10条 帮助 条数/页： 5101520253035404550556065707580859095100 排序方式： 请选择题名升序题名降序提交时间升序提交时间降序作者升序作者降序发表日期升序发表日期降序 Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor 期刊论文  OAI收割 JOURNAL OF PROPULSION AND POWER, 2023 作者:  Wu ZJ(吴振杰);  Zhang QF(张启帆);  Yu FY(于方游);  Luo WH(罗苇航);  Gao ZB(高占彪)   |  收藏  |  浏览/下载：25/0  |  提交时间：2023/06/15 Scramjet Engines  Combustor Design  flame stabilization mode  transition  path dependence   Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor 期刊论文  OAI收割 AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11 作者:  Liu, Mingjiang;  Sun, Mingbo;  Zhao, Guoyan;  Meng Y(孟宇);  Huang, Yuhui   |  收藏  |  浏览/下载：45/0  |  提交时间：2022/12/20 Tandem-cavity  Scramjet combustor  Combustion mode  Thrust performance   Investigation for Effects of Jet Scale on Flame Stabilization in Scramjet Combustor 期刊论文  OAI收割 ENERGIES, 2022, 卷号: 15, 期号: 10, 页码: 16 作者:  Li, Zhen;  Gu, Hongbin;  Gu HB(顾洪斌);  Li Z(李桢)   |  收藏  |  浏览/下载：32/0  |  提交时间：2022/07/18 scramjet combustor  direct-connect test  jet scale  flame stabilization   Improved delayed detached eddy simulation of supersonic combustion fueled by liquid kerosene 期刊论文  OAI收割 FUEL, 2022, 卷号: 313, 页码: 13 作者:  Shen, Wubingyi;  Huang, Yue;  Yao, Wei;  Liu, Hedong;  You, Yancheng   |  收藏  |  浏览/下载：66/0  |  提交时间：2022/05/17 Improved delayed detached eddy simulation  Liquid kerosene  Skeletal reaction mechanism  Equivalence ratio  Cavity-based scramjet combustor  Supersonic combustion   Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文  OAI收割 Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: 1-8 作者:  Gu HB(顾洪斌);  Yue LJ(岳连捷);  Gao ZB(高占彪)   |  收藏  |  浏览/下载：42/0  |  提交时间：2019/10/15 Scramjet Combustor Mode Transition Liquid Kerosene Acceleration   Development of Skeletal Kerosene Mechanisms and Application to Supersonic Combustion 期刊论文  OAI收割 ENERGY & FUELS, 2018, 页码: 10.1021/acs.energyfuels.8b03350 作者:  Yao W(姚卫);  Wu K(吴坤);  Fan XJ(范学军)   |  收藏  |  浏览/下载：37/0  |  提交时间：2018/12/27 Combustion Condition  Combustor Efficiency  Improved Delayed Detached Eddy Simulations  Initial Temperatures  Laminar Flame Speed  Scramjet Combustors  Supersonic Combustion  Turbulence-chemistry Interactions   Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文  OAI收割 AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175 作者:  Wang ZP(王知溥);  Li F(李飞);  Gu HS;  Yu XL(余西龙);  Zhang XY(张新宇) 收藏  |  浏览/下载：39/0  |  提交时间：2015/06/12 Scramjet  Dual-mode combustor  Divergent angle  Cavity location  Combustion efficiency  TDLAS   Uncertainty in velocity measurement based on diode-laser absorption in nonuniform flows 期刊论文  OAI收割 APPLIED OPTICS, 2012, 卷号: 51, 期号: 20, 页码: 4788-4797 作者:  Li F(李飞);  Yu XL(余西龙);  Cai WW;  Ma L 收藏  |  浏览/下载：38/0  |  提交时间：2013/01/18 Wavelength-Modulation Spectroscopy  Water-Vapor  Temperature Distributions  Scramjet Combustor  Gas Temperature  Parameters  Pressure  Sensors   A compact sensor based on near infrared absorption spectroscopy for flow diagnostics in a low density hydrogen and oxygen combustion driven shock tube 期刊论文  OAI收割 Lasers in Engineering, 2012, 卷号: 23, 期号: 1-2, 页码: 1-17 作者:  Yu XL(余西龙);  Li F(李飞);  Chen LH(陈立红);  Chang XY(张新宇) 收藏  |  浏览/下载：29/0  |  提交时间：2012/12/04 tunable diode-laser  water-vapor  scramjet combustor  temperature  gases  H2O  CO  oh  tunable diode laser absorption spectroscopy (tdlas)  combustion  rapid time-division-multiplexing (tdm)  temperature  water vapour concentration  low density shock tube   Experimental investigation on the cavity-based scramjet model 期刊论文  OAI收割 CHINESE SCIENCE BULLETIN, 2009, 卷号: 54, 期号: 16, 页码: 2794-2799 作者:  Gu HB(顾洪斌);  Chen LH(陈立红);  Zhang XY(张新宇);  Gu HB(顾洪斌) 收藏  |  浏览/下载：778/81  |  提交时间：2009/09/28 scramjet  combustor  cavity  performance