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Date Issued:2021
Community:高温气体动力学国家重点实验室
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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, Yunfeng
;
Wang, Chun
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Submit date:2022/01/24
基于被动内窥火焰传感器技术的超声速燃烧感知实验研究
学位论文
硕士论文,北京: 中国科学院大学, 2021
Authors:
李忠朋
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Submit date:2022/01/12
内窥光纤传感器
超声速燃烧感知
火焰自发光
水基与煤油基纳米流体导热及对流传热特性研究
学位论文
博士论文,北京: 中国科学院大学, 2021
Authors:
范文慧
Adobe PDF(8784Kb)
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Submit date:2022/01/12
纳米流体
航空煤油
导热性能
对流传热性能
努塞尔数
RBCC发动机引射模态流态分析及性能研究
学位论文
博士论文,北京: 中国科学院大学, 2021
Authors:
陈 科挺
Adobe PDF(10651Kb)
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Submit date:2022/01/11
RBCC
引射模态
流动形态
流动匹配
简化建模
Error Analysis of Integrated Absorbance for TDLAS in a Nonuniform Flow Field
期刊论文
APPLIED SCIENCES-BASEL, 2021, 卷号: 11, 期号: 22, 页码: 15
Authors:
Li RJ(李仁杰)
;
Li F(李飞)
;
Lin X(林鑫)
;
Yu XL(余西龙)
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Submit date:2022/01/13
TDLAS
integrated absorbance
error analysis
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
Experimental study on shock wave control in high-enthalpy hypersonic flow by using SparkJet actuator
期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 416-425
Authors:
Xie, Wei
;
Luo, Zhenbing
;
Zhou, Yan
;
Gao, Tianxiang
;
Wu, Yun
;
Wang Q(汪球)
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Submit date:2022/10/25
SparkJet
High-enthalpy hypersonic flow
Shock control
Shock-on-shock interaction
Air supply
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
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
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