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一种拓展超声速燃烧火焰稳定极限的方法 专利
发明专利. 一种拓展超声速燃烧火焰稳定极限的方法, 专利号: ZL201310410973.8, 申请日期: 2013-09-11, 授权日期: 2015-10-14
Inventors:  张泰昌;  王晶;  范学军
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Wave system fitting: A new method for force measurements in shock tunnels with long test duration 期刊论文
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2015, 卷号: 62-63, 页码: 2841-2848
Authors:  Luo CT(罗长童);  Wang YP(汪云鹏);  Wang C(王春);  Jiang ZL(姜宗林);  Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(1074Kb)  |  Favorite  |  View/Download：356/99  |  Submit date：2016/01/07
Aerodynamic Force Measurements  Strain Gauge Balance  Inertia Compensation  Signal Decomposition  Accelerometer-free  Shock Tunnels  
一种主动冷却亚燃冲压发动机燃油切换的系统和方法 专利
发明专利. 一种主动冷却亚燃冲压发动机燃油切换的系统和方法, 专利号: ZL201310451746.X, 申请日期: 2013-09-27, 授权日期: 2015-09-27
Inventors:  袁涛;  陆阳;  李龙;  王晶;  孟令瑾;  范学军
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Numerical study of oblique detonation wave initiation in a stoichiometric hydrogen-air mixture 期刊论文
PHYSICS OF FLUIDS, 2015, 卷号: 27, 期号: 9, 页码: 96101
Authors:  Wang T;  Zhang YN;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Ng HD;  Wang, T (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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一种以加热煤油为燃料的超声速燃烧室 专利
发明专利. 一种以加热煤油为燃料的超声速燃烧室, 专利号: ZL201310411204.X, 申请日期: 2013-09-11, 授权日期: 2015-07-08
Inventors:  张泰昌;  王晶;  范学军
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Relative contribution ratio: A quantitative metrics for multi-parameter analysis 期刊论文
Cogent Mathematics, 2015, 卷号: 2, 期号: 1, 页码: 1068979
Authors:  Luo CT(罗长童);  Jiang ZL(姜宗林);  Wang C(王春);  Hu ZM(胡宗民)
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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：457/94  |  Submit date：2016/01/08
Hydrocarbons  Combustors  Cooling  Heat Transfer  
H_2O/CO_2污染对RP-3航空煤油着火特性的影响 期刊论文
推进技术, 2015, 卷号: 36, 期号: 3, 页码: 336-344
Authors:  梁金虎;  王苏;  张灿;  张胜涛;  岳连捷;  范秉诚;  张新宇;  崔季平
View  |  Adobe PDF(1583Kb)  |  Favorite  |  View/Download：253/66  |  Submit date：2015/12/25
污染效应  着火延时  煤油  H2o  Co2  激波管  
On the numerical technique for the simulation of hypervelocity test flows 期刊论文
Computers & Fluids, 2015, 卷号: 106, 页码: 12-18
Authors:  Hu ZM(胡宗民);  Wang C(王春);  Jiang ZL(姜宗林);  Khoo BC;  Hu ZM(胡宗民)
View  |  Adobe PDF(1617Kb)  |  Favorite  |  View/Download：1585/922  |  Submit date：2014/11/27
Hypervelocity Test Flow  Dcd Scheme  Flux-splitting  Spurious Oscillation  
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:  Yao W(姚卫);  Wang J(王晶);  Lu Y(陆阳);  Li XP(李晓鹏);  Fan XJ(范学军)
Adobe PDF(1195Kb)  |  Favorite  |  View/Download：492/177  |  Submit date：2016/07/01
Adiabatic Flame Temperature  Combustion  Directed Graphs  Flow Separation  Heat Flux  Kerosene  Large Eddy Simulation  Musculoskeletal System  Real Time Systems  Sensitivity Analysis  Spacecraft  Transients