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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.
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：1185/288  |  Submit date：2012/04/01
Flow rate analyses and calibrations of kerosene cracking for supersonic combustion 会议论文
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, United states, July 10, 2005 - July 13, 2005
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国)
View  |  Adobe PDF(315Kb)  |  Favorite  |  View/Download：261/69  |  Submit date：2017/06/01
Average Molecular Weight  Chemical Formulae  Cracking Model  Gaseous Products  High Temperature  Ideal Gas Law  Ideal Gas Mixtures  Mass Flow Rate  Mole Fraction  Residence Time  Room Temperature  Sonic Nozzle  Supercritical Condition  Supersonic Combustion  Temperature Dependencies  Thermal Cracking  Three-component