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Knowledge Management System of Institue of Mechanics, CAS
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Community:高温气体动力学国家重点实验室
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Effect of helical fins on the combustion performance in a micro-step combustor
期刊论文
FUEL, 2022, 卷号: 319, 页码: 13
Authors:
Zhang Z(张政)
;
Shen WBY
;
Yao W(姚卫)
;
Wang Q(汪球)
;
Zhao W(赵伟)
Adobe PDF(11881Kb)
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Submit date:2022/05/17
Micro-combustion
Helical fin
Combustion performance
Conjugate heat transfer
Mixing
高超声速高焓条件下的内嵌式温敏漆测量方法
期刊论文
力学学报, 2022, 卷号: 54, 期号: 01, 页码: 48-58
Authors:
苑朝凯
;
姜宗林
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Submit date:2022/03/16
温敏漆
热流密度场
辐射效应
高超声速流动
辨识方法
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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Submit date:2022/10/25
Boundary layer combustion
Skin-friction reduction
Supersonic combustion
Scramjet engine
Comparison of Strategies for Coupled Flow-Thermal Analysis of Thermal Protection System at Hypersonic Flight Condition
期刊论文
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 卷号: 21, 期号: 2, 页码: 347-362
Authors:
Wang RX(王睿星)
;
Wang, ZW
;
Zheng HW(郑洪伟)
;
Song HW(宋宏伟)
Adobe PDF(4182Kb)
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Submit date:2020/06/22
Coupled flow-thermal analysis
Thermal protection system
Basic direct correction method (BDCM)
Improved DCM (IDCM)
Iteration solution method (ISM)
Enhancement of combustion performance in a microchannel: Synergistic effects of bluff-body and cavity
期刊论文
FUEL, 2020, 卷号: 265, 页码: 11
Authors:
Zhang Z
;
Wu K(吴坤)
;
Yao W(姚卫)
;
Yuen R
;
Wang J
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Submit date:2020/04/07
Micro-combustor
Bluff-body
Cavity
Combustion performance
Flame-flow interaction
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:
Fan WH(范文慧)
;
Zhong FQ(仲峰泉)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
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Submit date:2020/03/11
Wall heat flux
Numerical simulation
Ethylene
Supersonic combustor
CH* Luminance Distribution Application and a One-Dimensional Model of the Supersonic Combustor Heat Release Quantization
期刊论文
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2019, 卷号: 36, 期号: 1, 页码: 45-50
Authors:
Wang ZP(王知溥)
;
Gu HB(顾洪斌)
;
Cheng L W
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
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Submit date:2019/04/11
supersonic combustion
one-dimensional modelling
heat release
CH* chemiluminescence
基于工程转捩模型的高超声速进气道特性
期刊论文
北京航空航天大学学报, 2018, 卷号: 44, 期号: 7, 页码: 1408-1418
Authors:
杨慧
;
路文睿
;
李虹杨
;
岳连捷
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Submit date:2018/10/24
高超声速进气道
转捩模型
飞行高度
湍流度
数值模拟
Inverse estimation of near-field temperature and surface heat flux via single point temperature measurement
期刊论文
HEAT AND MASS TRANSFER, 2017, 卷号: 53, 期号: 2, 页码: 439-450
Authors:
Wu CW(吴臣武)
;
Shu YH(舒勇华)
;
Xie JJ(谢季佳)
;
Jiang JZ(蒋建政)
;
Fan J(樊菁)
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Submit date:2017/04/26
Development of a radiative heating system for studies of heat transfer in fuel-cooled structures
会议论文
14th International Energy Conversion Engineering Conference, Salt Lake City, UT, JUL 25-27, 2016
Authors:
Dong D(董达)
;
Lu Y(陆阳)
;
Yuan YM(袁越明)
;
Fan XJ(范学军)
;
Dong, D (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Submit date:2017/05/12
Aviation Kerosene
Supercritical Conditions
Pressure
Rp-3