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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
Authors:  Jin YC(靳一超);  Wu K(吴坤);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1121Kb)  |  Favorite  |  View/Download：180/49  |  Submit date：2022/07/04
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：510/109  |  Submit date：2018/12/26
Development of a radiative heating system for studies of heat transfer in fuel-cooled structures 会议论文
14th International Energy Conversion Engineering Conference, Salt Lake City, UT, JUL 25-27, 2016
Authors:  Dong D(董达);  Lu Y(陆阳);  Yuan YM(袁越明);  Fan XJ(范学军);  Dong, D (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
View  |  Adobe PDF(637Kb)  |  Favorite  |  View/Download：313/82  |  Submit date：2017/05/12
Aviation Kerosene  Supercritical Conditions  Pressure  Rp-3  
Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
Authors:  Lu Y(陆阳);  Wang XZ(王新竹);  Li L(李龙);  Cheng D(程迪);  Yuan T(袁涛);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(445Kb)  |  Favorite  |  View/Download：480/98  |  Submit date：2016/01/08
Hydrocarbons  Combustors  Cooling  Heat Transfer  
Visualization of Vaporized Kerosene Combustion in a Supersonic Combustor Using Pulsed Schlieren System 会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Atlanta, Georgia, July 30-Augest 1, 2012
Authors:  Yuan YM(袁越明);  Yang M(杨猛);  Zhang TC(张泰昌);  Yu G(俞刚);  Fan XJ(范学军)
View  |  Adobe PDF(1965Kb)  |  Favorite  |  View/Download：848/286  |  Submit date：2013/03/05
A Thermal Analysis Method for Fuel-Cooled Combustor Structure based on Heat Flux Measurement 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference., Tours,France, 2012.9.24-28
Authors:  Lu Y(陆阳);  Li L(李龙);  Fan XJ(范学军)
View  |  Adobe PDF(483Kb)  |  Favorite  |  View/Download：1020/379  |  Submit date：2013/02/28
Three-Dimensional heat transfer analysis and optimized design of actively cooled strut for scramjet applications 会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
Authors:  Zhong FQ(仲峰泉);  Chen TY(陈同银);  Fan XJ(范学军);  Chen LH(陈立红);  Zhang XY(张新宇);  Zhong FQ(仲峰泉)
View  |  Adobe PDF(2023Kb)  |  Favorite  |  View/Download：562/118  |  Submit date：2014/02/24
Characteristics of a supersonic model combustor with two-staged injections of supercritical kerosene 会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
Authors:  Zhang TC(张泰昌);  Yuan YM(袁越明);  Li JG(李建国);  Fan XJ(范学军);  Zhang TC(张泰昌)
View  |  Adobe PDF(636Kb)  |  Favorite  |  View/Download：570/164  |  Submit date：2014/02/24
Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions 会议论文
AIAA/ASME/SAE/ASEE 45th Joint Propulsion Conference and Exhibit, Denver, CO, AUG 02-08, 2009
Authors:  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Sung CJ;  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
View  |  Adobe PDF(57Kb)  |  Favorite  |  View/Download：1181/288  |  Submit date：2012/04/01
采用简化机理模拟乙烯在超声速气流中自点火燃烧过程 会议论文
第三届高超声速科技学术会议, 江苏·无锡
Authors:  仲峰泉;  范学军;  俞刚;  张新宇
Adobe PDF(830Kb)  |  Favorite  |  View/Download：1007/266  |  Submit date：2010/11/25