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| Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor 期刊论文
JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 5, 页码: 11
Authors: Cheng D(程迪) ; Wang J(王晶); Lu Y(陆阳); Li L(李龙); Yao W(姚卫); Fan XJ(范学军)
 View |  Adobe PDF(2651Kb) |  Favorite | View/Download：414/135 | Submit date：2019/09/09
Heat flux measurement Kerosene Supersonic combustion Scramjet Heat flux sensor |
| 一种用于超声速然烧的直连台的气膜冷却装置 专利
发明专利. 一种用于超声速然烧的直连台的气膜冷却装置, 专利号: ZL201611135726.1, 申请日期: 2016-12-12,
Inventors: 樊川; 王晶; 孟令瑾; 范学军
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| Modeling Analysis of an Actively Cooled Scramjet Combustor Under Different Kerosene/Air Ratios 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 4, 页码: 975-991
Authors: Yao W(姚卫); Lu Y(陆阳); Wu K(吴坤); Wang J(王晶); Fan XJ(范学军)
View | Adobe PDF(2427Kb) | Favorite | View/Download：373/114 | Submit date：2018/10/19 |
| 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
Authors: 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)
View | Adobe PDF(807Kb) | Favorite | View/Download：354/111 | Submit date：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
Authors: 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)
View | Adobe PDF(805Kb) | Favorite | View/Download：409/153 | Submit date：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
Authors: 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)
View | Adobe PDF(1173Kb) | Favorite | View/Download：462/225 | Submit date：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
Authors: Fan C(樊川); Wang J(王晶); Fan XJ(范学军)
View | Adobe PDF(735Kb) | Favorite | View/Download：327/109 | Submit date：2018/01/16
Combustion Combustors Coolants Kerosene Spacecraft Supersonic Aerodynamics |
| 超声速燃烧实验的煤油流量控制装置 专利
发明专利. 超声速燃烧实验的煤油流量控制装置, 专利号: ZL201310449424.1, 申请日期: 2013-09-24, 授权日期: 2016-05-25
Inventors: 李龙; 王晶; 孟令瑾; 王景全; 黄鹏; 范学军
View | Adobe PDF(1111Kb) | Favorite | View/Download：382/53 | Submit date：2016/06/12 |
| 一种应用于超声速燃烧试验的电气设备控制电路 专利
发明专利. 一种应用于超声速燃烧试验的电气设备控制电路, 专利号: ZL201310438784.1, 申请日期: 2013-08-21, 授权日期: 2016-05-04
Inventors: 李龙; 王晶; 张泰昌; 袁涛; 王景泉; 范学军
View | Adobe PDF(1434Kb) | Favorite | View/Download：301/58 | Submit date：2016/05/17 |
| 超声速燃烧试验的煤油流量控制方法 专利
发明专利. 超声速燃烧试验的煤油流量控制方法, 专利号: ZL201310436804.1, 申请日期: 2013-09-24, 授权日期: 2016-04-13
Inventors: 李龙; 王晶; 程迪; 袁涛; 范学军
View | Adobe PDF(1123Kb) | Favorite | View/Download：279/43 | Submit date：2016/04/18 |
