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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
Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow
期刊论文
AIAA JOURNAL, 2022, 页码: 9
Authors:
Wu ZJ(吴振杰)
;
Zhang QF(张启帆)
;
Zhang X(张旭)
;
Luo WH(罗苇航)
;
Gao ZB(高占彪)
;
Yue LJ(岳连捷)
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Submit date:2022/07/18
Energy-based drag decomposition analyses for a turbulent channel flow developing over convergent-divergent riblets
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 2, 页码: 16
Authors:
Guo TB(郭同彪)
;
Fang,Jian
;
Zhong,Shan
;
Moulinec,Charles
Adobe PDF(9532Kb)
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Submit date:2022/03/28
Hysteresis of Shock Train Movement in the Isolator with a Ramp
期刊论文
AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882
Authors:
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang P
;
Zhao QJ
Adobe PDF(2961Kb)
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Submit date:2022/02/17
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
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:
Zhou GX(周功喜)
;
Zhang X(张旭)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Zhang SZ(张仕忠)
;
Lin X(林鑫)
;
Li F(李飞)
;
Chen H(陈宏)
;
Yue LJ(岳连捷)
;
Yu XL(余西龙)
Adobe PDF(4108Kb)
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Submit date:2021/09/07
High mach number scramjet
Circular cross-section
TDLAS
Multi-view simultaneous imaging
POD
Theoretical, numerical and experimental study of hypersonic boundary layer transition: Blunt circular cone
期刊论文
APPLIED THERMAL ENGINEERING, 2021, 卷号: 194, 页码: 14
Authors:
Chen, Jianqiang
;
Yi, Shihe
;
Li XL(李新亮)
;
Han GL(韩桂来)
;
Zhang, Yifeng
;
Yang, Qiang
;
Yuan, Xianxu
Adobe PDF(11175Kb)
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Submit date:2021/08/03
Hypersonic boundary layer
Stability
Transition
Thermal protection
Specific signal imaging velocimetry for rarefied plasma flows
期刊论文
EXPERIMENTS IN FLUIDS, 2020, 卷号: 61, 期号: 12, 页码: 247
Authors:
Cao JW(曹进文)
;
Huang HJ(黄河激)
;
Pan WX(潘文霞)
;
Meng X(孟显)
;
Wu CK(吴承康)
Adobe PDF(4736Kb)
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Submit date:2020/12/28
MOLECULAR TAGGING VELOCIMETRY
MACH PROBE
VELOCITY
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