IMECH-IR

Browse/Search Results:  1-10 of 18 Help

Filters            
Selected(0)Clear Items/Page:    Sort:
Characteristics of cellular structure of detonation waves propagating in annular channels 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 10, 页码: 13
Authors:  Yao KP(姚克鹏);  Yang PF(杨鹏飞);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(8005Kb)  |  Favorite  |  View/Download:45/4  |  Submit date:2024/02/19
Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  Favorite  |  View/Download:408/77  |  Submit date:2022/08/24
Multistage Launch Vehicle  Aerodynamic Characteristics  Shock Wave Interaction  Angle of Attack  Waverider  Boundary Layer Flow  Total Variation Diminishing  Adverse Pressure Gradient  Hypersonic Flows  Hypersonic Wind Tunnels  
Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文
AIAA JOURNAL, 2021, 页码: 12
Authors:  Lin MY(林明月);  Wang C(王春);  Peng J(彭俊);  Jiang ZL(姜宗林)
Adobe PDF(4805Kb)  |  Favorite  |  View/Download:326/60  |  Submit date:2022/01/12
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  Favorite  |  View/Download:290/61  |  Submit date:2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
The Role of Three-Dimensional Shock Wave Interaction in the Complex Hypersonic Heating 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:  Wang C(王春);  Xiang GX(项高翔);  Jiang ZL(姜宗林);  Li XD(李旭东);  Shi CM(师曾敏)
View  |  Adobe PDF(376Kb)  |  Favorite  |  View/Download:360/69  |  Submit date:2020/01/06
Three-dimensional shock wave configurations induced by two asymmetrical intersecting wedges in supersonic flow 期刊论文
SHOCK WAVES, 2018, 卷号: 28, 期号: 2, 页码: 311-319
Authors:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(腾宏辉);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1333Kb)  |  Favorite  |  View/Download:560/148  |  Submit date:2018/10/30
Supersonic Flow  3d Shock/shock Interaction  3d Asymmetrical Wave Configurations  Spatial Dimension Reduction  
Shock/shock interactions between bodies and wings 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
Authors:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(腾宏辉);  Jiang ZL(姜宗林)
View  |  Adobe PDF(1161Kb)  |  Favorite  |  View/Download:318/76  |  Submit date:2018/10/30
Body And Wing  Flow Field  Hypersonic Flow  Shock/shock Interaction  Wave Configurations  
THE MECHANISM OF THREE-DIMENSION STEADY SHOCK WAVE INTERACTION 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors:  Wang C(王春);  Yang RX(杨瑞欣);  Jiang ZL(姜宗林)
View  |  Adobe PDF(3021Kb)  |  Favorite  |  View/Download:233/71  |  Submit date:2019/04/19
Investigations of Three-Dimensional Shock/Shock Interactions over Symmetrical Intersecting Wedges 期刊论文
AIAA JOURNAL, 2016, 卷号: 54, 期号: 5, 页码: 1472-1481
Authors:  Xiang GX(项高翔);  Wang C(王春);  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(578Kb)  |  Favorite  |  View/Download:482/167  |  Submit date:2016/09/14
Ceramics  Thermal Shock  Size Effect  
Theoretical solutions to three-dimensional asymmetrical shock/shock interaction 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 8, 页码: 1208-1216
Authors:  Xiang GX(项高翔);  Wang C(王春);  Hu ZM(胡宗民);  Li XD;  Jiang ZL(姜宗林);  Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
View  |  Adobe PDF(995Kb)  |  Favorite  |  View/Download:500/122  |  Submit date:2016/12/08
3d Asymmetrical Shock/shock Interaction  Spatial-dimension Reduction  Mach Reflection  Flow Field  Theoretical Analysis