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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 作者: Yao W(姚卫); Chen L(陈留) Adobe PDF(2272Kb)  |  收藏  |  浏览/下载:264/145  |  提交时间:2021/06/11 |
| 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) 浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载:263/90  |  提交时间:2018/01/16 Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 作者: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军); Zhang, Peng(pengzhang.zhang@polyu.edu.hk) 浏览  |  Adobe PDF(1249Kb)  |  收藏  |  浏览/下载:300/89  |  提交时间:2018/01/16 Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
| 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) 浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载:275/82  |  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 |
| Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor 会议论文 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015 作者: Lu Y(陆阳); Wang XZ(王新竹); Li L(李龙); Cheng D(程迪); Yuan T(袁涛); Yao W(姚卫); Fan XJ(范学军) Adobe PDF(445Kb)  |  收藏  |  浏览/下载:427/92  |  提交时间:2016/01/08 Hydrocarbons Combustors Cooling Heat Transfer |
| Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition 会议论文 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012 作者: Xiao YB(肖雅彬); Yue LJ(岳连捷); Chen LH(陈立红); Zhang XY(张新宇); Xiao YB(肖雅彬) 浏览  |  Adobe PDF(1674Kb)  |  收藏  |  浏览/下载:431/112  |  提交时间:2014/02/24 |
| Modeling and measurements of heat release distributions in dual-mode scramjet combustor 会议论文 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012 作者: Tian L(田璐); Chen LH(陈立红); Chen Q(陈强); Li F(李飞); Zhang XY(张新宇); Tian L(田璐) 浏览  |  Adobe PDF(677Kb)  |  收藏  |  浏览/下载:615/195  |  提交时间:2014/02/24 |
| High beam quality 400W practical all-solid-state laser for laser beam texture 会议论文 High-Power Lasers and Applications V, Beijing, China, October 18, 2010 - October 19, 2010 作者: Geng AC(耿爱丛); Yang MJ(杨明江); Zhao C; Li BH; Geng, A. (aicong_77@126.com) 浏览  |  Adobe PDF(243Kb)  |  收藏  |  浏览/下载:219/80  |  提交时间:2017/06/20 1064 Nm All Solid-state Lasers Beam Quality Factor Birefringence Compensation High Beam Quality Low Concentrations Nd:Yag Crystal Nd:Yag Laser Optical Conversion Efficiency Output Power Pump Power Side-pumped Unstable Resonators |