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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
作者:  Li B(李波);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1358Kb)  |  收藏  |  浏览/下载：152/46  |  提交时间：2021/02/01
Influence of compressibility effect on supersonic combustion modeling 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
作者:  Chen L;  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1280Kb)  |  收藏  |  浏览/下载：159/72  |  提交时间：2020/11/20
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：263/90  |  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：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  
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Yao W(姚卫);  Wang J(王晶);  Lu Y(陆阳);  Li XP(李晓鹏);  Fan XJ(范学军)
Adobe PDF(1195Kb)  |  收藏  |  浏览/下载：474/173  |  提交时间：2016/07/01
Adiabatic Flame Temperature  Combustion  Directed Graphs  Flow Separation  Heat Flux  Kerosene  Large Eddy Simulation  Musculoskeletal System  Real Time Systems  Sensitivity Analysis  Spacecraft  Transients  
A comparative study of highly underexpanded nitrogen and hydrogenjets using large eddy simulation 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Li XP(李晓鹏);  Wu K(吴坤);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(728Kb)  |  收藏  |  浏览/下载：276/89  |  提交时间：2017/05/05
Comparative Studies  Flow Charac  Teristics  High Order Harmonics  High Resolution  Instability Modes  Near  Field Structure  Shock Structure  Under  Expanded Jets  
Three-dimensional numerical study of the acoustic properities of a highly underexpanded jet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Wu K(吴坤);  Li XP(李晓鹏);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(590Kb)  |  收藏  |  浏览/下载：365/92  |  提交时间：2017/05/05
Frequency Spectrum Analysis  High Temporal Resolution  Instantaneous Flow  Noise Generation Mechanisms  Theoretical Modeling  Three  Dimensional Numerical Studies  Transport Mechanism  Under  Expanded Jets