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一种并联两级入轨飞行器纵向分离方案的数值研究 期刊论文
航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634
Authors:  王粤;  汪运鹏;  王春;  姜宗林
Adobe PDF(4901Kb)  |  Favorite  |  View/Download：609/92  |  Submit date：2022/07/11
两级入轨  高超声速  纵向分离  气动干扰  非定常流动  
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：421/79  |  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  
Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(9707Kb)  |  Favorite  |  View/Download：329/96  |  Submit date：2022/11/14
Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference  
TSTO马赫7安全级间分离问题的数值研究 期刊论文
力学学报, 2022, 卷号: 54, 期号: 2, 页码: 526-542
Authors:  王粤;  汪运鹏;  薛晓鹏;  姜宗林
Adobe PDF(3565Kb)  |  Favorite  |  View/Download：388/80  |  Submit date：2021/12/23
两级入轨  高超声速  分离流动  气动干扰  级间分离  
Impulse force-measurement system 期刊论文
SHOCK WAVES, 2020, 页码: 11
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(1551Kb)  |  Favorite  |  View/Download：269/81  |  Submit date：2020/11/30
Shock tunnel  High enthalpy  Aerodynamic force measurement  Strain gauge balance  
超声速三维进气道内激波干扰的研究 期刊论文
推进技术, 2017, 期号: 12, 页码: 6
Authors:  项高翔;  王春;  汪运鹏;  姜宗林
View  |  Adobe PDF(1393Kb)  |  Favorite  |  View/Download：496/107  |  Submit date：2017/12/22
高超声速流动  箱式进气道  侧壁压缩进气道  波系结构  流场区域  
Starting Process in a Large-Scale Shock Tunnel 期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
Authors:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
View  |  Adobe PDF(764Kb)  |  Favorite  |  View/Download：357/98  |  Submit date：2017/09/19
Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
Authors:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
View  |  Adobe PDF(5104Kb)  |  Favorite  |  View/Download：260/50  |  Submit date：2017/05/05
Inviscid Flows  Numerical Investigations  Outlet Diameters  Reflected Shock Waves  Simulated Results  Starting Process  Transmitted Shock  Unsteady Nozzle Flow