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Indexed By:SCI
Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
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Detonation wave structure and thrust variation of a ram accelerator with different projectile velocities
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 143, 页码: 8
Authors:
Shang JH(尚甲豪)
;
Wang, Kuanliang
;
Wang, Aifeng
;
Wang Q(汪球)
;
Zhao W(赵伟)
Adobe PDF(4127Kb)
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View/Download:104/14
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Submit date:2024/01/02
Ram accelerator
Detonation
Oblique detonation wave
Recirculation zone
Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11
Authors:
Liu, Mingjiang
;
Sun, Mingbo
;
Zhao, Guoyan
;
Meng Y(孟宇)
;
Huang, Yuhui
;
Ma, Guangwei
;
Wang, Hongbo
Adobe PDF(3841Kb)
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View/Download:118/26
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Submit date:2022/12/20
Tandem-cavity
Scramjet combustor
Combustion mode
Thrust performance
On jet-wake flame stabilization in scramjet: A LES/RANS study from chemical kinetic and fluid-dynamical perspectives
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 120, 页码: 12
Authors:
Wu K(吴坤)
;
Zhang, Peng
;
Fan XJ(范学军)
Adobe PDF(3834Kb)
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View/Download:363/59
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Submit date:2022/01/24
Supersonic combustion
Jet-wake flame stabilization
Hybrid LES
RANS
Detailed hydrogen chemistry
Counter-rotating vortex pair
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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View/Download:289/109
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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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View/Download:298/72
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21
Authors:
Yang L(杨磊)
;
Ye, Zhengyin
;
Li WH(李文皓)
;
Sun QH(孙泉华)
Adobe PDF(4621Kb)
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View/Download:286/63
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Submit date:2021/11/01
Store separation
Aerodynamic modeling
Interference aerodynamics
Dynamic simulation
Air-launch-to-orbit
Reduction of surface friction drag in scramjet engine by boundary layer combustion
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
Authors:
Xue, Rui
;
Zheng, Xing
;
Yue LJ(岳连捷)
;
Zhang, Qian
;
He, Xin
;
Yang, Jing
;
Weng, Chao
;
Li, Zhihao
Adobe PDF(5483Kb)
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View/Download:156/48
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Submit date:2022/10/25
Boundary layer combustion
Skin-friction reduction
Supersonic combustion
Scramjet engine
Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 112, 页码: 9
Authors:
Wang KL(王宽亮)
;
Yang PF(杨鹏飞)
;
Teng HH(滕宏辉)
Adobe PDF(2853Kb)
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Submit date:2021/05/17
Oblique detonation
Wave complex
Instability
Thermal choking
Expansion corner
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:
Tong XT(仝晓通)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(8067Kb)
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View/Download:413/75
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Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
Authors:
Zhang ZJ(张子健)
;
Ma KF(马凯夫)
;
Zhang WS(张文硕)
;
Han X(韩鑫)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(2608Kb)
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View/Download:275/117
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Submit date:2020/11/30
Oblique detonation engine
Pre-injection
Detonative combustion
Mixing
Hydrogen