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Atomization of misaligned impinging liquid jets 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 9, 页码: 15
作者:  Zhang, Chenwei;  Zhang ZY(张振宇);  Wu K(吴坤);  Xia, Xi;  Fan XJ(范学军)
Adobe PDF(15401Kb)  |  收藏  |  浏览/下载：232/48  |  提交时间：2022/01/12
AMP Exception  AMP Exception  
A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels 会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
作者:  Jin YC(靳一超);  Wu K(吴坤);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1121Kb)  |  收藏  |  浏览/下载：150/42  |  提交时间：2022/07/04
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 3, 页码: 772-786
作者:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
浏览  |  Adobe PDF(807Kb)  |  收藏  |  浏览/下载：334/103  |  提交时间：2018/07/17
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
作者:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
浏览  |  Adobe PDF(805Kb)  |  收藏  |  浏览/下载：389/145  |  提交时间：2018/06/06
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：438/216  |  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  
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：298/89  |  提交时间：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
Characterization of flame stabilization modes in an ethylene-fueled supersonic combustor using time-resolved CH* chemiluminescence 期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017, 卷号: 36, 期号: 2, 页码: 2919-2925
作者:  Yuan YM(袁越明);  Zhang TC(张泰昌);  Yao W(姚卫);  Fan XJ(范学军);  Zhang P(张鹏);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, PR, Peoples R China.
浏览  |  Adobe PDF(1681Kb)  |  收藏  |  浏览/下载：318/94  |  提交时间：2017/12/27
Supersonic Combustion  Flame Stabilization  Stagtnation Temperature  Gloabal Equivalence Ratio  Ch** Ch*emiluminesenCh*e  
Development of integrated high temperature sensor for simultaneous measurement of wall heat flux and temperature 期刊论文
REVIEW OF SCIENTIFIC INSTRUMENTS, 2012, 卷号: 83, 期号: 7, 页码: 074901
作者:  Li L(李龙);  Wang J(王晶);  Fan XJ(范学军);  Fan, XJ;  Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
Adobe PDF(2757Kb)  |  收藏  |  浏览/下载：1235/337  |  提交时间：2013/01/18
Radiative Calibration  Facilities  Cavity  Gauge  Meter  Nist