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超声速三维进气道内激波干扰的研究 期刊论文
推进技术, 2017, 期号: 12, 页码: 6
作者:  项高翔;  王春;  汪运鹏;  姜宗林
浏览  |  Adobe PDF(1393Kb)  |  收藏  |  浏览/下载：470/96  |  提交时间：2017/12/22
高超声速流动  箱式进气道  侧壁压缩进气道  波系结构  流场区域  
Experimental and Numerical Study on Hypersonic Flow over Double-Wedge Configuration 期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 9, 页码: 3227-3230
作者:  Meng BQ(孟宝清);  Han GL(韩桂来);  Yuan CK(苑朝凯);  Wang C(王春);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(207Kb)  |  收藏  |  浏览/下载：452/111  |  提交时间：2018/01/04
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
作者:  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.
浏览  |  Adobe PDF(419Kb)  |  收藏  |  浏览/下载：428/114  |  提交时间：2017/10/27
Effect of HCl on NO Formation during CO/NH3 Combustion in an Entrained Flow Reactor at 1023-1223 K 期刊论文
ENERGY & FUELS, 2017, 卷号: 31, 期号: 3, 页码: 3281-3287
作者:  Wang Y(王阳);  Zhao J;  Wei XL(魏小林);  Li S(李森);  Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Wei, XL (reprint author), Univ Chinese Acad Sci, Sch Sci & Engn, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1719Kb)  |  收藏  |  浏览/下载：333/77  |  提交时间：2017/07/24
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：441/217  |  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  
Experimental Studies of Film Cooling in Supersonic Combustors 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Fan C(樊川);  Wang J(王晶);  Fan XJ(范学军)
浏览  |  Adobe PDF(735Kb)  |  收藏  |  浏览/下载：309/102  |  提交时间：2018/01/16
Combustion  Combustors  Coolants  Kerosene  Spacecraft  Supersonic Aerodynamics  
Force Test in a Large-Scale Shock Tunnel 会议论文
55th AIAA Aerospace Sciences Meeting , Grapevine, Texas, 9-13 January 2017
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(6096Kb)  |  收藏  |  浏览/下载：308/89  |  提交时间：2018/01/16
INFLUENCE OF HIGH ALTITUDE ON COMBUSTION EFFICIENCY AND RADIATION FRACTION OF HYDROCARBON FIRES 期刊论文
HEAT TRANSFER RESEARCH, 2017, 卷号: 48, 期号: 10, 页码: 865-875
作者:  Li HH;  Yao W(姚卫);  Li P;  Zhou ZH;  Wang J
浏览  |  Adobe PDF(1193Kb)  |  收藏  |  浏览/下载：362/122  |  提交时间：2017/11/29
Hydrocarbon Fire  Heat Release Rate  Combustion Efficiency  Radiation Fraction  Transmittance  
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
作者:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(679Kb)  |  收藏  |  浏览/下载：387/68  |  提交时间：2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis