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基于主动射流控制的高超声速进气道再起动性能研究（英文） 期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors:  靳一超;  姚卫
Adobe PDF(1844Kb)  |  Favorite  |  View/Download：174/41  |  Submit date：2023/02/09
高超声速进气道  不起动  再起动  主动射流  流动控制  
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：328/95  |  Submit date：2022/11/14
Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference  
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  Favorite  |  View/Download：330/88  |  Submit date：2022/08/23
Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering  
Advances in Plasma Diagnostics and Applications 专著
Beijing:MDPI, 2022
Authors:  Editors：Chen ZT;  Attri P;  Wang Q(汪球)
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Characterization of reflected shock tunnel air conditions using a simple method 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 5, 页码: 17
Authors:  Gu, Sangdi;  Olivier, Herbert;  Wen, Chih-Yung;  Hao, Jiaao;  Wang Q(汪球)
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Numerical and Experimental Study on the Duration of Nozzle Starting of the Reflected High-Enthalpy Shock Tunnel 期刊论文
APPLIED SCIENCES-BASEL, 2022, 卷号: 12, 期号: 6, 页码: 16
Authors:  Yu JP(于江鹏);  Li JP(李进平);  Wang Q(汪球);  Zhang XY(张晓源);  Zhang SZ(张仕忠)
Adobe PDF(6583Kb)  |  Favorite  |  View/Download：345/153  |  Submit date：2022/05/17
nozzle starting  high-enthalpy shock tunnel  center startup  complete startup  
Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
Authors:  Jiang ZL(姜宗林);  Teng, Honghui
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Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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Boundary layer correction  High-enthalpy flow  Hypersonic wind tunnel  Nozzle design  Real-gas effects