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Numerical Simulation Research on Thermal Response Characteristics of E-type Coaxial Thermocouples 会议论文
2021 2rd International Conference on Applied Mechanics and Mechanical Engineering, 长沙, 2021/09/12
Authors:  Qi L(齐力);  Han GL(韩桂来);  Jiang ZL(姜宗林)
Favorite  |  View/Download：93/0  |  Submit date：2022/07/06
气动热  同轴热电偶  数值模拟  
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
Authors:  Li B(李波);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1358Kb)  |  Favorite  |  View/Download：172/55  |  Submit date：2021/02/01
Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:  Yao W(姚卫);  Li B(李波)
Adobe PDF(1665Kb)  |  Favorite  |  View/Download：170/51  |  Submit date：2020/11/20
Dynamic zone flamelet model  GH2/GO2  Large Eddy Simulation (LES)  Rocket combustor  Turbulence-chemistry interaction  
Supercritical GN2/GH2 jet modeled by the ECS method 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:  Yao W(姚卫);  Jin YC(靳一超);  Lee YC(李亚超)
Adobe PDF(1048Kb)  |  Favorite  |  View/Download：186/73  |  Submit date：2020/11/20
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
Authors:  Chen L;  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1280Kb)  |  Favorite  |  View/Download：192/77  |  Submit date：2020/11/20
Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
Authors:  Wang Y;  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(1120Kb)  |  Favorite  |  View/Download：516/111  |  Submit date：2018/12/26
Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
View  |  Adobe PDF(679Kb)  |  Favorite  |  View/Download：418/79  |  Submit date：2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis  
Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor 会议论文
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
Authors:  Cheng D(程迪);  Wang J(王晶);  Gong J;  Lu Y(陆阳);  Yao W(姚卫);  Li L(李龙);  Fan XJ(范学军);  Fan, Xuejun (xfan@imech.ac.cn)
View  |  Adobe PDF(2131Kb)  |  Favorite  |  View/Download：350/127  |  Submit date：2017/05/05
Equivalence Ratios  Heat Flux Distributions  Heat Transfer Characteristics  Scramjet  Supercritical Kerosenes  Supersonic Combustion  Supersonic Combustors  Total Temperatures