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岳连捷 [4]
张启帆 [3]
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黄庭隆 [3]
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Funding Organization:National Natural Science Foundation of China
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Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition
期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
Authors:
Zhang WS(张文硕)
;
Zhang, Zijian
;
Jiang ZL(姜宗林)
;
Han X(韩信)
;
Liu YF(刘云峰)
;
Wang C(王春)
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Submit date:2022/01/24
Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy
期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
Authors:
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Peng JL(彭锦龙)
;
Liu, Yan
;
Zhang ZL(张泽林)
;
Fang SH(方思晗)
;
Yu XL(余西龙)
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Submit date:2021/11/01
Hybrid rocket engine
Fuel mass flow rate
Tunable diode laser absorption spectroscopy
Temperature
Partial pressure
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
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Submit date:2022/02/17
Combustion Characteristic and Mechanism of a Mixture Working Fluid C3H8/CO2
期刊论文
JOURNAL OF THERMAL SCIENCE, 2021, 页码: 12
Authors:
Shi Weixiu
;
Pan LS(潘利生)
;
Jin Suyi
;
Dong YH(董跃华)
;
Li T(李腾)
;
Zhao J(赵京)
;
Wei XL(魏小林)
Adobe PDF(2198Kb)
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Submit date:2021/11/01
CO2-based mixture
flammability
laminar flame speed
flammable critical mixing ratio
transcritical power cycle
Fluid-structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system
期刊论文
NONLINEAR DYNAMICS, 2021, 页码: 22
Authors:
Zhu, Hong
;
Sun, Qinglin
;
Liu, Xuefeng
;
Liu, Jinglei
;
Sun, Hao
;
Wu WN(邬婉楠)
;
Tan, Panlong
;
Chen, Zengqiang
Adobe PDF(4213Kb)
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Submit date:2021/08/03
Fluid-structure interaction
Parafoil system
Flexible deformation
Trailing edge deflection
Aerodynamic performance
Dynamic model
Numerical study on the shock/combustion interaction of oblique detonation waves
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
Authors:
Yang L
;
Yue LJ(岳连捷)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
Adobe PDF(5176Kb)
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Submit date:2020/11/30
Oblique detonation wave
Shock/combustion interaction
Shock polar analysis
High-resolution simulation
Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
Authors:
Zhang X(张旭)
;
Yue LJ(岳连捷)
;
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
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Submit date:2020/03/21
Hysteresis
Dual-mode scramjet
Supersonic combustion
Mode transition
Flame stabilization
Combustion oscillation
Investigation on the cycle performance and the combustion characteristic of two CO2-based binary mixtures for the transcritical power cycle
期刊论文
ENERGY, 2019, 卷号: 179, 页码: 454-463
Authors:
Pan LS(潘利生)
;
Ma YJ
;
Li T(李腾)
;
Li HX(李慧鑫)
;
Li B
;
Wei XL(魏小林)
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Submit date:2019/09/09
CO2-Based mixtures
Transcritical power cycle
Waste heat recovery
Flammability
Numerical study of a fully confined supersonic slot impinging jet from bleed system
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Chang XY(张新宇)
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View/Download:547/177
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Submit date:2019/09/09
Fully confined supersonic jet
Inclined impingement
Heat transfer
Boundary layer bleed
Numerical simulation
Numerical simulation of the interaction of two shear layers in double backward-facing steps
期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 5, 页码: 15
Authors:
Deng F(邓放)
;
Han GL(韩桂来)
;
Liu MK(刘美宽)
;
Ding, J
;
Weng, PF
;
Jiang ZL(姜宗林)
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Submit date:2019/10/21