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On the response of coaxial surface thermocouples for transient aerodynamic heating measurements 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2017, 卷号: 86, 页码: 141-148
Authors:  Li JP(李进平);  Chen H(陈宏);  Zhang SZ(张仕忠);  Zhang XY(张晓源);  Yu HR(俞鸿儒);  Chen, H (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1158Kb)  |  Favorite  |  View/Download：502/110  |  Submit date：2017/07/24
Heat Flux Measurement  Thermocouple  Response Characteristics  Shock Tube  
An Experimental Study of Chilton-Colburn Analogy Between Turbulent Flow and Convective Heat Transfer of Supercritical Kerosene 期刊论文
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2017, 卷号: 139, 期号: 6
Authors:  Zhang YJ(张永江);  Zhong FQ(仲峰泉);  Xing YF(邢云绯);  张新宇 Xinyu;  Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Bei Si Huan Xi Rd 15, Beijing 100190, Peoples R China.;  Zhong, FQ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
View  |  Adobe PDF(1041Kb)  |  Favorite  |  View/Download：460/121  |  Submit date：2017/07/24
Aviation Kerosene  Supercritical  Skin Friction Coefficient  Convective Heat Transfer  Chilton-colburn Analogy  
Influence of Thermal Sensor Installation on Measuring Accuracy at Stagnation Points 期刊论文
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2017, 卷号: 31, 期号: 2, 页码: 318-323
Authors:  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
View  |  Adobe PDF(419Kb)  |  Favorite  |  View/Download：446/117  |  Submit date：2017/10/27
A low-dissipation solver based on OpenFOAM designed for large eddy simulation in compressible flows 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(1377Kb)  |  Favorite  |  View/Download：303/117  |  Submit date：2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems  
A low-dissipation scheme based on OpenFoam designed for large eddy simulation in compressible flow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军);  Yao, Wei(weiyao@imech.ac.cn)
View  |  Adobe PDF(1358Kb)  |  Favorite  |  View/Download：446/114  |  Submit date：2018/01/16
Computational Fluid Dynamics  Computer Software  Digital Storage  Kinetic Energy  Kinetics  Open Source Software  Open Systems  Runge Kutta Methods  Shock Tubes  Shock Waves  Spacecraft  Turbulence  Two Phase Flow  
A low-dissipation solver based on openFOAM designed for large eddy simulation in compressible flow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
Authors:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(1377Kb)  |  Favorite  |  View/Download：509/104  |  Submit date：2018/11/08
Computational Fluid Dynamics  Digital Storage  Kinetic Energy  Kinetics  Open Source Software  Open Systems  Ramjet Engines  Runge Kutta Methods  Shock Tubes  Turbulence  Two Phase Flow  Bench  Mark Problems  Central  Upwind Scheme  Computational Fluid Dynamics Software  Skew  Symmetric Forms  Temporal Discretization  Turbulence Structures  Unstructured Meshes  Wall Bounded Turbulence  
Inverse estimation of near-field temperature and surface heat flux via single point temperature measurement 期刊论文
HEAT AND MASS TRANSFER, 2017, 卷号: 53, 期号: 2, 页码: 439-450
Authors:  Wu CW(吴臣武);  Shu YH(舒勇华);  Xie JJ(谢季佳);  Jiang JZ(蒋建政);  Fan J(樊菁)
View  |  Adobe PDF(3874Kb)  |  Favorite  |  View/Download：618/111  |  Submit date：2017/04/26
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)
Adobe PDF(679Kb)  |  Favorite  |  View/Download：411/77  |  Submit date：2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis