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姜宗林 [7]
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Influence of non-thermal plasma and electric field on non-premixed methane flame
期刊论文
THERMAL SCIENCE AND ENGINEERING PROGRESS, 2024, 卷号: 47, 页码: 15
Authors:
Zhang YF(张玉锋)
;
Li T(李腾)
;
Wei XL(魏小林)
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Submit date:2024/03/11
Non -thermal plasma
Coaxial micro -tube burner
Methane flame
Combustion stability
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)
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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)
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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)
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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
Numerical and Experimental Study on Vertical Takeoff and Separation of the Compound Aircraft
期刊论文
IEEE ACCESS, 2022, 卷号: 10, 页码: 47597-47617
Authors:
Wang D
;
Hong QZ(洪启臻)
;
Huang X(黄鑫)
;
Pei XB
;
Wang J
Adobe PDF(4750Kb)
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Submit date:2022/07/18
Aircraft
Aircraft propulsion
Compounds
Aerodynamics
Engines
Automotive components
Tail
Compound aircraft
CFD
vertical take-off
dynamical separation of two aircraft
Design of a milli-newton force balance for hypersonic rarefied wind tunnel
期刊论文
MEASUREMENT, 2021, 卷号: 185, 页码: 7
Authors:
Wu CW(吴臣武)
;
Liu C(刘聪)
;
Hu DL(胡灯亮)
;
Liu HL(刘宏立)
;
Huang HJ(黄河激)
Adobe PDF(4178Kb)
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Submit date:2021/11/15
Strain
Balance
Milli-newton
Design
Calibration
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:
Li, Mengzhe
;
Wang, Zhikai
;
Xu, Rongguang
;
Zhang, Xiaoliang
;
Chen, Zhitong
;
Wang Q(汪球)
Adobe PDF(8841Kb)
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Submit date:2021/11/01
Non-equilibrium plasma
Plasma-assisted ignition
Plasma-assisted combustion
Aerospace engine
Combustor
Extreme condition
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:
Yao W(姚卫)
;
Liu H(刘杭)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
Adobe PDF(2954Kb)
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
A sharp interface immersed boundary method for flow-induced noise prediction using acoustic perturbation equations
期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 227, 页码: 15
Authors:
Zhao, Cheng
;
Yang Y(杨焱)
;
Zhang, Tao
;
Dong, Haibo
;
Hou, Guoxiang
Adobe PDF(3919Kb)
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Submit date:2021/08/30
Acoustic perturbation equations
Immersed boundary method
Flow-induced noise
Four-cylinder array
Parametric Study on Lateral–Directional Stability of Hypersonic Waverider
期刊论文
AIAA Journal, 2021, 卷号: 59, 期号: 8, 页码: 3025-3042
Authors:
刘文
;
张陈安
;
Wang Xiao-Peng
;
Li Jin-Jie
;
王发民
Adobe PDF(7528Kb)
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Submit date:2021/08/30