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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：156/72  |  提交时间：2020/11/20
On the application of tabulated dynamic adaptive chemistry in ethylene-fueled supersonic combustion 期刊论文
COMBUSTION AND FLAME, 2018, 卷号: 197, 页码: 265-275
作者:  Wu K(吴坤);  Contino F;  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(4270Kb)  |  收藏  |  浏览/下载：515/178  |  提交时间：2018/12/12
Tabulated dynamic adaptive chemistry  Skeletal mechanism  Supersonic combustion  Ethylene  Large Eddy Simulation  
Modeling Analysis of an Actively Cooled Scramjet Combustor Under Different Kerosene/Air Ratios 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 4, 页码: 975-991
作者:  Yao W(姚卫);  Lu Y(陆阳);  Wu K(吴坤);  Wang J(王晶);  Fan XJ(范学军)
浏览  |  Adobe PDF(2427Kb)  |  收藏  |  浏览/下载：353/106  |  提交时间：2018/10/19
Numerical investigation of characteristic frequency excited highly underexpanded jets 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 304-316
作者:  Li XP;  Fan E;  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
浏览  |  Adobe PDF(3588Kb)  |  收藏  |  浏览/下载：441/141  |  提交时间：2017/07/24
Fuel Jets  Underexpanded Jets  Jet Mixing Control  Excited Jets  Large Eddy Simulation  
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 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);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Fan XJ(范学军);  Fan, Xuejun(xfan@imech.ac.cn)
浏览  |  Adobe PDF(1173Kb)  |  收藏  |  浏览/下载：440/216  |  提交时间：2018/01/16
Adiabatic Flame Temperature  Aerodynamics  Boundary Layer Flow  Boundary Layers  Chemical Analysis  Combustion  Computational Chemistry  Directed Graphs  Flow Separation  Mach Number  Principal Component Analysis  Regression Analysis  Sensitivity Analysis  Spacecraft  Supersonic Aerodynamics  Supersonic Aircraft  Transients  
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：273/81  |  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  
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：472/172  |  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